Relevant bibliographies by topics / Boundary-Layer Instability

Academic literature on the topic 'Boundary-Layer Instability'

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Published: 10 December 2022
Last updated: 28 January 2023

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Journal articles on the topic "Boundary-Layer Instability"

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Kerschen, E. J. "Boundary Layer Receptivity Theory." Applied Mechanics Reviews 43, no. 5S (May 1, 1990): S152—S157. http://dx.doi.org/10.1115/1.3120795.

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The receptivity mechanisms by which free-stream disturbances generate instability waves in laminar boundary layers are discussed. Free-stream disturbances have wavelengths which are generally much longer than those of instability waves. Hence, the transfer of energy from the free-stream disturbance to the instability wave requires a wavelength conversion mechanism. Recent analyses using asymptotic methods have shown that the wavelength conversion takes place in regions of the boundary layer where the mean flow adjusts on a short streamwise length scale. This paper reviews recent progress in the theoretical understanding of these phenomena.
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Staley, D. O. "Boundary-Layer Damping of Baroclinic Instability." Journal of the Atmospheric Sciences 50, no. 5 (March 1993): 772–77. http://dx.doi.org/10.1175/1520-0469(1993)050<0772:bldobi>2.0.co;2.

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NASH, EMMA C., MARTIN V. LOWSON, and ALAN McALPINE. "Boundary-layer instability noise on aerofoils." Journal of Fluid Mechanics 382 (March 10, 1999): 27–61. http://dx.doi.org/10.1017/s002211209800367x.

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An experimental and theoretical investigation has been carried out to understand the tonal noise generation mechanism on aerofoils at moderate Reynolds number. Experiments were conducted on a NACA0012 aerofoil section in a low-turbulence closed working section wind tunnel. Narrow band acoustic tones were observed up to 40 dB above background noise. The ladder structure of these tones was eliminated by modifying the tunnel to approximate to anechoic conditions. High-resolution flow velocity measurements have been made with a three-component laser-Doppler anemometer (LDA) which have revealed the presence of strongly amplified boundary-layer instabilities in a region of separated shear flow just upstream of the pressure surface trailing edge, which match the frequency of the acoustic tones. Flow visualization experiments have shown these instabilities to roll up to form a regular Kármán-type vortex street.A new mechanism for tonal noise generation has been proposed, based on the growth of Tollmien–Schlichting (T–S) instability waves strongly amplified by inflectional profiles in the separating laminar shear layer on the pressure surface of the aerofoil. The growth of fixed frequency, spatially growing boundary-layer instability waves propagating over the aerofoil pressure surface has been calculated using experimentally obtained boundary-layer characteristics. The effect of boundary-layer separation has been incorporated into the model. Frequency selection and prediction of T–S waves are in remarkably good agreement with experimental data.
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Parziale, N. J., J. E. Shepherd, and H. G. Hornung. "Observations of hypervelocity boundary-layer instability." Journal of Fluid Mechanics 781 (September 16, 2015): 87–112. http://dx.doi.org/10.1017/jfm.2015.489.

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A novel optical method is used to measure the high-frequency (up to 3 MHz) density fluctuations that precede transition to turbulence within a laminar boundary layer in a hypervelocity flow. This optical method, focused laser differential interferometry, enables measurements of short-wavelength, high-frequency disturbances that are impossible with conventional instrumentation such as pressure transducers or hot wires. In this work, the T5 reflected-shock tunnel is used to generate flows in air, nitrogen and carbon dioxide with speeds between 3.5 and $5~\text{km}~\text{s}^{-1}$ (Mach numbers between 4 and 6) over a 5° half-angle cone at zero angle of attack. Simultaneous measurements are made at two locations approximately midway along a generator of the 1-m-long cone. With increasing Reynolds number (unit values were between 2 and $5\times 10^{6}~\text{m}^{-1}$), density fluctuations are observed to grow in amplitude and transition from a single narrow band of frequencies consistent with the Mack or second mode of boundary-layer instability to bursts of large-amplitude and spectrally broad disturbances that appear to be precursors of turbulent spots. Disturbances that are sufficiently small in initial amplitude have a wavepacket-like signature and are observed to grow in amplitude between the upstream and downstream measurement locations. A cross-correlation analysis indicates propagation of wavepackets at speeds close to the edge velocity. The free stream flow created by the shock tunnel and the resulting boundary layer on the cone are computed, accounting for chemical and vibrational non-equilibrium processes. Using this base flow, local linear and parabolized stability (PSE) analyses are carried out and compared with the experimental results. Reasonable agreement is found between measured and predicted most unstable frequencies, with the greatest differences being approximately 15 %. The scaling of the observed frequency with the inverse of boundary-layer thickness and directly with the flow velocity are consistent with the characteristics of Mack’s second mode, as well as results of previous researchers on hypersonic boundary layers.
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Grenier, Emmanuel, Yan Guo, and Toan T. Nguyen. "Spectral instability of characteristic boundary layer flows." Duke Mathematical Journal 165, no. 16 (November 2016): 3085–146. http://dx.doi.org/10.1215/00127094-3645437.

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Thompson, Charles, Vineet Mehta, and Arun Mulpur. "Secondary instability of a Stokes boundary layer." Journal of the Acoustical Society of America 91, no. 4 (April 1992): 2352. http://dx.doi.org/10.1121/1.403459.

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Roberts, P. J. D., J. M. Floryan, G. Casalis, and D. Arnal. "Boundary layer instability induced by surface suction." Physics of Fluids 13, no. 9 (September 2001): 2543–52. http://dx.doi.org/10.1063/1.1384868.

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Craig, Stuart A., and William S. Saric. "Crossflow instability in a hypersonic boundary layer." Journal of Fluid Mechanics 808 (October 27, 2016): 224–44. http://dx.doi.org/10.1017/jfm.2016.643.

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The crossflow instability in a hypersonic, laminar boundary layer is investigated using point measurements inside the boundary layer for the first time. Experiments are performed on a 7° right, circular cone with an adiabatic wall condition at 5.6° angle of incidence in the low-disturbance Mach 6 Quiet Tunnel at Texas A&M University. Measurements are made with a constant-temperature hot-wire anemometer system with a frequency response up to 180 kHz. Stationary crossflow waves are observed to grow and saturate. A travelling wave coexists with the stationary wave and occurs in a frequency band centred around 35 kHz. A type-I secondary instability is also observed in a frequency band centred around 110 kHz. The behaviour of all three modes is largely consistent with their low-speed counterparts prior to saturation of the stationary wave. Afterward, the behaviour remains in partial agreement with the low-speed case. Neither type-II secondary instability nor transition to turbulence are observed in this study.
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Gudkov, V. A. "Effect of instability on boundary layer detachment." Journal of Applied Mechanics and Technical Physics 32, no. 5 (1992): 703–6. http://dx.doi.org/10.1007/bf00851938.

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de Luca, L., G. Cardone, D. Aymer de la Chevalerie, and A. Fonteneau. "Goertler instability of a hypersonic boundary layer." Experiments in Fluids 16, no. 1 (November 1993): 10–16. http://dx.doi.org/10.1007/bf00188500.

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Dissertations / Theses on the topic "Boundary-Layer Instability"

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Nash, Emma Clare. "Boundary layer instability noise on aerofoils." Thesis, University of Bristol, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.337698.

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Imayama, Shintaro. "Studies of the rotating-disk boundary-layer flow." Doctoral thesis, KTH, Strömningsfysik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-158973.

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The rotating-disk boundary layer is not only a simpler model for the study of cross-flow instability than swept-wing boundary layers but also a useful simplification of many industrial-flow applications where rotating configurations are present. For the rotating disk, it has been suggested that a local absolute instability, leading to a global instability, is responsible for the small variation in the observed laminar-turbulent transition Reynolds number however the exact nature of the transition is still not fully understood. This thesis aims to clarify certain aspects of the transition process. Furthermore, the thesis considers the turbulent rotating-disk boundary layer, as an example of a class of three-dimensional turbulent boundary-layer flows. The rotating-disk boundary layer has been investigated in an experimental apparatus designed for low vibration levels and with a polished glass disk that gave a smooth surface. The apparatus provided a low-disturbance environment and velocity measurements of the azimuthal component were made with a single hot-wire probe. A new way to present data in the form of a probability density function (PDF) map of the azimuthal fluctuation velocity, which gives clear insights into the laminar-turbulent transition region, has been proposed. Measurements performed with various disk-edge conditions and edge Reynolds numbers showed that neither of these conditions a↵ect the transition process significantly, and the Reynolds number for the onset of transition was observed to be highly reproducible. Laminar-turbulent transition for a ‘clean’ disk was compared with that for a disk with roughness elements located upstream of the critical Reynolds number for absolute instability. This showed that, even with minute surface roughness elements, strong convectively unstable stationary disturbances were excited. In this case, breakdown of the flow occurred before reaching the absolutely unstable region, i.e. through a convectively unstable route. For the rough disk, the breakdown location was shown to depend on the amplitude of individual stationary vortices. In contrast, for the smooth (clean-disk) condition, the amplitude of the stationary vortices did not fix the breakdown location, which instead was fixed by a well-defined Reynolds number. Furthermore, for the clean-disk case, travelling disturbances have been observed at the onset of nonlinearity, and the associated disturbance profile is in good agreement with the eigenfunction of the critical absolute instability. Finally, the turbulent boundary layer on the rotating disk has been investigated. The azimuthal friction velocity was directly measured from the azimuthal velocity profile in the viscous sublayer and the velocity statistics, normalized by the inner scale, are presented. The characteristics of this three-dimensional turbulent boundary-layer flow have been compared with those for the two-dimensional flow over a flat plate and close to the wall they are found to be quite similar but with rather large differences in the outer region.

QC 20150119

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Imayama, Shintaro. "Experimental study of the rotating-disk boundary-layer flow." Licentiate thesis, KTH, Mekanik, 2012. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-95147.

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Rotating-disk flow has been investigated not only as a simple model of cross flow instability to compare with swept-wing flow but also for industrial flow applications with rotating configurations. However the exact nature of laminar-turbulent transi- tion on the rotating-disk flow is still major problem and further research is required for it to be fully understood, in particular, the laminar-turbulent transition process with absolute instability. In addition the studies of the rotating-disk turbulent boundary- layer flow are inadequate to understand the physics of three-dimensional turbulent boundary-layer flow. In present thesis, a rotating-rotating disk boundary-layer flow has been inves- tigated experimentally using hot-wire anemometry. A glass disk with a flat surface has been prepared to archieve low disturbance rotating-disk environment. Azimuthal velocity measurements using a hot-wire probe have been taken for various conditions. To get a better insight into the laminar-turbulent transition region, a new way to describe the process is proposed using the probability density function (PDF) map of azimuthal fluctuation velocity. The effect of the edge of the disk on the laminar-turbulent transition process has been investigated. The disturbance growth of azimuthal fluctuation velocity as a function of Reynolds number has a similar trend irrespective of the various edge conditions. The behaviour of secondary instability and turbulent breakdown has been in- vestigated. It has been found that the kinked azimuthal velocity associated with secondary instability just before turbulent breakdown became less apparent at a cer- tain wall normal heights. Furthermore the turbulent breakdown of the stationary mode seems not to be triggered by its amplitude, however, depend on the appearance of the travelling secondary instability. Finally, the turbulent boundary layer on a rotating disk has been investigated. An azimuthal friction velocity has been directly measured from the azimuthal velocity profile in the viscous sub-layer. The turbulent statistics normalized by the inner and outer sclaes are presented.
QC 20120529
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Masad, Jamal A. "On subharmonic instability in boundary layers." Thesis, Virginia Tech, 1987. http://hdl.handle.net/10919/45783.

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The subharmonic instability in two-dimensional boundary layer on a flat plate is analyzed using the parametric instability model and the resonant triad model. The problems arising from both models are solved numerically using the shooting technique and results are presented. It is found that in the presence of a strong interaction (e.g., large amplitude of the two-dimensional wave), results from the resonant triad model are inaccurate as compared with the experimental data and the t results from the parametric instability model. This is mainly because the resonant triad model is a weakly nonlinear model, and it does not account for the modification of the eigenfunctions of the interacting waves which really takes place as we find out from the experiments.

The parametric instability model is a powerful model, despite all the assumptions included. The model, however, does not introduce a clear understanding of how the subharmonic mode originates from the three-dimensional Tollmien-Schlichting modes.

For a weak interaction results from the resonant triad model and the parametric instability model get close to each other.


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Appelquist, Ellinor. "The rotating-disk boundary-layer flow studied through numerical simulations." Doctoral thesis, KTH, Mekanik, 2017. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-200827.

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This thesis deals with the instabilities of the incompressible boundary-layer flow thatis induced by a disk rotating in otherwise still fluid. The results presented include bothwork in the linear and nonlinear regime and are derived from direct numerical sim-ulations (DNS). Comparisons are made both to theoretical and experimental resultsproviding new insights into the transition route to turbulence. The simulation codeNek5000 has been chosen for the DNS using a spectral-element method (SEM) witha high-order discretization, and the results were obtained through large-scale paral-lel simulations. The known similarity solution of the Navier–Stokes equations for therotating-disk flow, also called the von K ́arm ́an rotating-disk flow, is reproduced by theDNS. With the addition of modelled small simulated roughnesses on the disk surface,convective instabilities appear and data from the linear region in the DNS are anal-ysed and compared with experimental and theoretical data, all corresponding verywell. A theoretical analysis is also presented using a local linear-stability approach,where two stability solvers have been developed based on earlier work. Furthermore,the impulse response of the rotating-disk boundary layer is investigated using DNS.The local response is known to be absolutely unstable and the global response, onthe contrary, is stable if the edge of the disk is assumed to be at radius infinity. Herecomparisons with a finite domain using various boundary conditions give a globalbehaviour that can be both linearly stable and unstable, however always nonlinearlyunstable. The global frequency of the flow is found to be determined by the Rey-nolds number at the confinement of the domain, either by the edge (linear case) or bythe turbulence appearance (nonlinear case). Moreover, secondary instabilities on topof the convective instabilities induced by roughness elements were investigated andfound to be globally unstable. This behaviour agrees well with the experimental flowand acts at a smaller radial distance than the primary global instability. The sharpline corresponding to transition to turbulence seen in experiments of the rotating diskcan thus be explained by the secondary global instability. Finally, turbulence datawere compared with experiments and investigated thoroughly.

QC 20170203

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Savin, Deborah Jane. "Linear and nonlinear aspects of interactive boundary layer transition." Thesis, University College London (University of London), 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.243306.

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Appelquist, Ellinor. "Direct numerical simulations of the rotating-disk boundary-layer flow." Licentiate thesis, KTH, Mekanik, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-146087.

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This thesis deals with the instabilities of the incompressible boundary-layer flow that is induced by a disk rotating in otherwise still fluid. The results presented are mostly limited to linear instabilities derived from direct numerical simulations (DNS) but with the objective that further work will focus on the nonlinear regime, providing greater insights into the transition route to turbulence. The numerical code Nek5000 has been chosen for the DNS using a spectral-element method in an effort to reduce spurious effects from low-order discretizations. Large-scale parallel simulations have been used to obtain the present results. The known similarity solution of the Navier–Stokes equation for the rotating-disk flow, also called the von Karman flow, is investigated and can be reproduced with good accuracy by the DNS. With the addition of small roughnesses on the disk surface, convective instabilities appear and data from the DNS are analysed and compared with experimental and theoretical data. A theoretical analysis is also presented using a local linear-stability approach, where two stability solvers have been developedbased on earlier work. A good correspondence between DNS and theory is found and the DNS results are found to explain well the behaviour of the experimental boundary layer within the range of Reynolds numbers for small amplitude (linear) disturbances. The comparison between the DNS and experimental results, presented for the first time here, shows that the DNS allows (for large azimuthal domains) a range of unstable azimuthal wavenumbers β to exist simultaneously with the dominantβ varying, which is not accounted for in local theory, where β is usually fixed for each Reynolds number at which the stability analysis is applied. Furthermore, the linear impulse response of the rotating-disk boundary layer is investigated using DNS. The local response is known to be absolutely unstable. The global response is found to be stable if the edge of the disk is assumed to be at infinity, and unstable if the domain is finite and the edge of the domain is placed such that there is a large enough pocket region for the absolute instability to develop. The global frequency of the flow is found to be determined by the edge Reynolds number.

QC 20140708

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8

Tyagi, P. K. "Linear Instability Of Laterally Strained Constant Pressure Boundary Layer Flows." Thesis, Indian Institute of Science, 2001. http://hdl.handle.net/2005/265.

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The linear instability of laterally diverging/converging flows is an important aspect towards understanding the laminar-transition process in many viscous flows. In this work the linear instability of constant pressure laterally diverging/converging flow has been investigated. The laminar velocity field for laterally diverging/converging flows, under the source/sink approximation, has been reduced to two-dimensional flows. This reduction is alternative to the Mangier transformation used earlier. For a constant pressure laterally strained flow, the laminar velocity is found to be governed by the Blasius equation for flow over a flat plate. The non-parallel linear instability of constant pressure laterally strained flows has been examined. The instability equation is found to be same as that for the Blasius flow. This implies that the stability is same as that for the Blasius flow. A lateral divergence/convergence is shown to alter the Reynolds number from that in a two-dimensional flow. The instability of a laterally converging/diverging flow thus can be obtained from the available results for the Blasius flow by scaling the Reynolds numbers. This leads to the result that while a diverging flow is more unstable than the Blasius flow, a converging flow is more stable. Some additional relevant results are also presented.
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Strange, Michael Edward. "The effect of surface cooling on compressible boundary-layer instability." Thesis, University of Hull, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.296279.

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Roland, Hannah. "Instability and receptivity of subsonic flow in the boundary layer." Thesis, Imperial College London, 2018. http://hdl.handle.net/10044/1/64819.

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In this thesis, the main focus is on the interaction of an incoming Tollmien–Schlichting wave with an isolated, stationary wall roughness in subsonic flow. In Part I, this problem is analysed by means of the Triple Deck theory. The linearised sublayer equations are solved under the assumption that the horizontal extent of the roughness is of O(L Re^(−3/8)) and that its height h is small, and an expression for the pressure perturbation is found. The transmission coefficient T_I , defined as the amplitude of the T–S wave downstream of the roughness divided by its initial amplitude, is then calculated, where |T_I | > 1 means that the wave is amplified and |T_I | < 1 represents an attenuation of the T–S wave. The transmission coefficient is dependent on the frequency ω, the height h of the roughness and on the Fourier transform of the roughness shape evaluated at zero value of the wavenumber. The same setup is investigated in Part II through numerical calculations: a DNS solver provides the base flows for 25 different gaps of varying width and height, which are then run through a PSE analysis to examine the stability of the flow. From the results of both methods it can be concluded that a surface indentation amplifies an incoming T–S wave, and that the amplification increases with the width and depth of the roughness. An additional geometry is studied in Part I by again employing the Triple Deck theory to investigate the effect small elastic vibrations of a semi-infinite plate attached to a stationary plate have on the boundary layer, and the receptivity coefficient is calculated for varying ω.
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Books on the topic "Boundary-Layer Instability"

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Seddougui, Sharon O. Surface-cooling effects on compressible boundary-layer instability. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

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El-Hady, Nabil M. Spatial three-dimensional secondary instability of compressible boundary-layer flows. Hampton, Va: Langley Research Center, 1989.

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Hall, Philip. On the instability of boundary layers on heated flat plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

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IUTAM Symposium (1993 Potsdam, N.Y.). Nonlinear instability of nonparallel flows. Berlin: Springer-Verlag, 1994.

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Hall, Philip. On the modulational instability of large amplitude waves in supersonic boundary layers. Hampton, VA: Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1995.

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Hall, Philip. The inviscid secondary instability of fully nonlinear longitudinal vortex structures in growing boundary layers. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

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Smith, A. Instability and transition of flow at, and near, an attachment-line: Including control by surface suction. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.

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Hall, Philip. An asymptotic investigation of the stationary modes of instability of the boundary layer on a rotating disc. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

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Canright, David. Rayleigh-Taylor instability of a viscous film overlying a pasive fluid. Monterey, Calif: Naval Postgraduate School, 1989.

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Seddougui, Sharon O. A nonlinear investigation of the stationary mode of instability of the three-dimensional compressible boundary layer due to a rotating disc. Hampton, Va: ICASE, 1989.

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Book chapters on the topic "Boundary-Layer Instability"

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Dovgal, A. V., V. V. Kozlov, and O. A. Simonov. "Experiments on Hydrodynamic Instability of Boundary Layers with Separation." In Boundary-Layer Separation, 109–30. Berlin, Heidelberg: Springer Berlin Heidelberg, 1987. http://dx.doi.org/10.1007/978-3-642-83000-6_7.

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Kachanov, Yury S. "Nonlinear Breakdown of Laminar Boundary Layer." In Nonlinear Instability of Nonparallel Flows, 21–51. Berlin, Heidelberg: Springer Berlin Heidelberg, 1994. http://dx.doi.org/10.1007/978-3-642-85084-4_2.

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Grosch, C. E., T. L. Jackson, and A. K. Kapila. "Nonseparable Eigenmodes of the Incompressible Boundary Layer." In Instability, Transition, and Turbulence, 127–36. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2956-8_13.

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Mankbadi, Reda R. "Boundary-Layer Transition: Critical-Layer Nonlinearity in Fully Interactive Resonant Triad." In Instability, Transition, and Turbulence, 216–30. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2956-8_21.

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Zang, Thomas A. "Aspects of Laminar Breakdown in Boundary-Layer Transition." In Instability, Transition, and Turbulence, 377–87. New York, NY: Springer New York, 1992. http://dx.doi.org/10.1007/978-1-4612-2956-8_37.

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Otto, A., and K. Nykyri. "Kelvin-Helmholtz instability and magnetic reconnection: Mass transport at the LLBL." In Earth's Low-Latitude Boundary Layer, 53–62. Washington, D. C.: American Geophysical Union, 2003. http://dx.doi.org/10.1029/133gm05.

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Healey, J. J. "Nonlinear Spatial Dynamics in a Growing Boundary Layer." In Nonlinear Instability of Nonparallel Flows, 127–36. Berlin, Heidelberg: Springer Berlin Heidelberg, 1994. http://dx.doi.org/10.1007/978-3-642-85084-4_10.

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Boiko, Andrey V., Alexander V. Dovgal, Genrih R. Grek, and Victor V. Kozlov. "Instability of the flat-plate boundary layer." In Physics of Transitional Shear Flows, 47–66. Dordrecht: Springer Netherlands, 2012. http://dx.doi.org/10.1007/978-94-007-2498-3_4.

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Khokhlov, A. P. "Asymptotic Analysis of Resonant Interactions in a Boundary Layer." In Nonlinear Instability of Nonparallel Flows, 81–85. Berlin, Heidelberg: Springer Berlin Heidelberg, 1994. http://dx.doi.org/10.1007/978-3-642-85084-4_5.

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Lin, Nay, Thomas A. Buter, David A. Fuciarelli, and Helen L. Reed. "Computational Aspects of Nonparallel Effects in Boundary-Layer Receptivity." In Nonlinear Instability of Nonparallel Flows, 98–105. Berlin, Heidelberg: Springer Berlin Heidelberg, 1994. http://dx.doi.org/10.1007/978-3-642-85084-4_7.

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Conference papers on the topic "Boundary-Layer Instability"

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Sanjose, Marlene, Prateek Jaiswal, Stephane Moreau, Aaron Towne, Sanjiva K. Lele, and Adrien Mann. "Laminar boundary layer instability noise." In 23rd AIAA/CEAS Aeroacoustics Conference. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2017. http://dx.doi.org/10.2514/6.2017-3190.

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Reshotko, Eli. "Boundary layer instability, transition and control." In 32nd Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-1.

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Marxen, Olaf, Thierry Magin, Gianluca Iaccarino, and Eric Shaqfeh. "Hypersonic Boundary-Layer Instability with Chemical Reactions." In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-707.

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Absi, Rafik. "WAVE BOUNDARY LAYER INSTABILITY NEAR FLOW REVERSAL." In Proceedings of the 28th International Conference. World Scientific Publishing Company, 2003. http://dx.doi.org/10.1142/9789812791306_0046.

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KOHAMA, Y. "Crossflow instability in rotating disk boundary-layer." In 19th AIAA, Fluid Dynamics, Plasma Dynamics, and Lasers Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1987. http://dx.doi.org/10.2514/6.1987-1340.

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Rienstra, Sjoerd, and Gregory Vilenski. "Spatial Instability of Boundary Layer Along Impedance Wall." In 14th AIAA/CEAS Aeroacoustics Conference (29th AIAA Aeroacoustics Conference). Reston, Virigina: American Institute of Aeronautics and Astronautics, 2008. http://dx.doi.org/10.2514/6.2008-2932.

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Robinet, Jean-Christophe, and P. Joubert de la Motte. "GLOBAL INSTABILITY IN SEPARATED INCOMPRESSIBLE LAMINAR BOUNDARY LAYER." In Third Symposium on Turbulence and Shear Flow Phenomena. Connecticut: Begellhouse, 2003. http://dx.doi.org/10.1615/tsfp3.510.

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Wang, Xiaowen, and Xiaolin Zhong. "Effect of Porous Coating on Boundary-Layer Instability." In 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2010. http://dx.doi.org/10.2514/6.2010-1243.

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Lowson, Martin, Alan McAlpine, and Emma Nash. "The generation of boundary layer instability noise on aerofoils." In 36th AIAA Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-627.

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Wu, Xuesong. "The role of acoustic feedback in boundary-layer instability." In 11TH INTERNATIONAL CONFERENCE OF NUMERICAL ANALYSIS AND APPLIED MATHEMATICS 2013: ICNAAM 2013. AIP, 2013. http://dx.doi.org/10.1063/1.4825481.

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Reports on the topic "Boundary-Layer Instability"

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Hornung, Hans G. Control of Boundary Layer Instability in Hypervelocity Flow. Fort Belvoir, VA: Defense Technical Information Center, January 2002. http://dx.doi.org/10.21236/ada400109.

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Zhong, Xiaolin. Direct Numerical Simulation and Experimental Validation of Hypersonic Boundary-Layer Receptivity and Instability. Fort Belvoir, VA: Defense Technical Information Center, March 2007. http://dx.doi.org/10.21236/ada467163.

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