Relevant bibliographies by topics / Aeroelasticity / Journal articles

Journal articles on the topic 'Aeroelasticity'

To see the other types of publications on this topic, follow the link: Aeroelasticity.
Author: Grafiati
Published: 4 June 2021
Last updated: 14 September 2024

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the top 50 journal articles for your research on the topic 'Aeroelasticity.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Browse journal articles on a wide variety of disciplines and organise your bibliography correctly.

1

Dowell, Earl, John Edwards, and Thomas Strganac. "Nonlinear Aeroelasticity." Journal of Aircraft 40, no. 5 (September 2003): 857–74. http://dx.doi.org/10.2514/2.6876.

Full text
APA, Harvard, Vancouver, ISO, and other styles
2

Li, Rui, and Chang Hong Tang. "Analysis for Nonlinear Aeroelasticity on Structure and its Current Progress." Advanced Materials Research 1022 (August 2014): 118–21. http://dx.doi.org/10.4028/www.scientific.net/amr.1022.118.

Full text
Abstract:
Firstly, the origin and mathematical mechanism of freeplay nonlinearity ,cubic nonlinearity, hysteresis nonlinearity was analyzed in this paper , and the importance of nonlinear aeroelasticity on structure was pointed out .On the current system of nonlinear aeroelasticity for the method of flutter analysis was summarized. Meanwhile on the mechanism of geometric nonlinearity and analytic methods have been studied, the future direction of the nonlinear aeroelasticity was concluded .
APA, Harvard, Vancouver, ISO, and other styles
3

S, Nithin, and Vijayalakshmi Bharathi K. "REVIEW ON AEROELASTICITY." International Journal of Engineering Applied Sciences and Technology 04, no. 08 (December 31, 2019): 271–74. http://dx.doi.org/10.33564/ijeast.2019.v04i08.047.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

TAMURA, Yukio, and Aakashi MOCHIDA. "INSTITUTE FOR AEROELASTICITY." Wind Engineers, JAWE 1987, no. 33 (1987): 113–16. http://dx.doi.org/10.5359/jawe.1987.33_113.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Da Ronch. "Special Issue: Aeroelasticity." Aerospace 6, no. 9 (August 23, 2019): 92. http://dx.doi.org/10.3390/aerospace6090092.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Bessert, N., and O. Frederich. "Nonlinear airship aeroelasticity." Journal of Fluids and Structures 21, no. 8 (December 2005): 731–42. http://dx.doi.org/10.1016/j.jfluidstructs.2005.09.005.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Tian, Shuling, Rongjie Li, and Ke Xu. "Investigation of Aeroelasticity Effect on Missile Separation from the Internal Bay." International Journal of Aerospace Engineering 2023 (February 16, 2023): 1–16. http://dx.doi.org/10.1155/2023/9875622.

Full text
Abstract:
There is a strong aerodynamic interference when launching the missile in the embedded mode. During the separation process, the carrier aircraft safety may be threatened due to large slenderness ratio, low structural stiffness, and aeroelasticity effects of the missile. The present study simulates missile separation in the presence of the aeroelasticity effects based on the computational fluid dynamics (CFD), rigid body dynamics (RBD), and computational structure dynamics (CSD) coupling method. A hybrid dynamic grid method consisting of the mixed overset unstructured grid and deformation grid is utilized. In order to verify the accuracy of the coupled numerical method, store separation from a wing and AGARD 445.6 wing flutter are first simulated as two standard test cases. The verification results imply that the present coupled numerical method is reliable and capable in simulation of the aeroelastic effect in missile separation. The influence of aeroelasticity on the separation trajectory of a missile from the internal bay is systematically studied at different states. Numerical results show that aeroelasticity substantially affects the missile angular displacement, while it has a slight impact on the linear displacement of the center of mass. Mach number and flight altitude are two important flight parameters that characterize the aeroelasticity effect on missile separation from the internal bay.
APA, Harvard, Vancouver, ISO, and other styles
8

Ye, Kun, Zhengyin Ye, Qing Zhang, and Zhan Qu. "Effects of aeroelasticity on the performance of hypersonic inlet." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 232, no. 11 (June 1, 2017): 2108–21. http://dx.doi.org/10.1177/0954410017710275.

Full text
Abstract:
Effects of the aeroelasticity on the performance of the hypersonic inlet have been investigated numerically in this study. The aeroelasticity has been simulated using the coupled computational fluid dynamics/computational structural dynamics method, which is solved by the in-house code. The unsteady Reynolds-averaged Navier–Stokes equations have been solved in the computational fluid dynamics simulation, and the modal method has been adopted in the computational structural dynamics simulation. Two cases have been utilized to validate the numerical method. Finally, the aeroelasticity has been simulated for inlet plate with different thicknesses. The effects of aeroelasticity on performance parameters and flow structure have been discussed in detail. The results show that the generalized displacements present the “beat” phenomenon in the time domain. The power spectral density of the generalized displacements implies that the aeroelastic instability is mainly caused by the coupling between the fourth- and fifth-order modes. The time-average flow rate coefficient and pressure rise ratio increase relative to the initial value, while the total pressure recovery coefficient decreases. The fluctuation amplitude of the flow rate coefficient is small, while that of the total pressure recovery coefficient and pressure rise ratio are relatively large. Besides, the phases of the three performance parameters are greatly different. Furthermore, the aeroelasticity has significant effect on the shock wave structure especially at the exit of the inlet.
APA, Harvard, Vancouver, ISO, and other styles
9

Li, Rui, and Chang Hong Tang. "Research and Application of Aeroelastic Analysis Based on Fluid-Structure Interaction." Advanced Materials Research 977 (June 2014): 418–22. http://dx.doi.org/10.4028/www.scientific.net/amr.977.418.

Full text
Abstract:
the origins and characteristics of linear and nonlinear aeroelasticity are analyzed.And the deforming mesh , fluid-structure coupling schemes, the design method of aerodynamic module and structure module interface are also analyzed. their advantages and disadvantages are Pointed out. Finally, several recommendations are given for the development orientation of aeroelasticity in the future.
APA, Harvard, Vancouver, ISO, and other styles
10

Fedorenko, Myhailo, and Oleksander Bondarenko. "Possibilities of the finite element method for the analysis of the aeroelasticity of the wing of a light aircraft." MECHANICS OF GYROSCOPIC SYSTEMS, no. 47 (May 15, 2024): 110–22. http://dx.doi.org/10.20535/0203-3771472024307685.

Full text
Abstract:
Modeling of the aeroelasticity of a straight wing for a light aircraft by the finite element method was carried out and the simulation results were verified by a binary model. The possibility of using the finite element method for modeling the aeroelasticity of a light-class aircraft is shown. A comparison of the aeroelasticity of a light aircraft wing with and without tapering was performed. The criterion for loss of wing stability during aeroelastic oscillations is the transition from a positive to a negative value of the damping coefficient in the wing-air system at a certain flight speed. Measures to strengthen the wing structure in order to ensure the necessary flight speed are indicated.
APA, Harvard, Vancouver, ISO, and other styles
11

SLOBODA, Oskar, Peter KORBA, Michal HOVANEC, and Jan PILA. "NUMERICAL APPROACH IN AEROELASTICITY." Scientific Journal of Silesian University of Technology. Series Transport 93 (December 1, 2016): 115–22. http://dx.doi.org/10.20858/sjsutst.2016.93.12.

Full text
APA, Harvard, Vancouver, ISO, and other styles
12

Livne, Eli. "Future of Airplane Aeroelasticity." Journal of Aircraft 40, no. 6 (November 2003): 1066–92. http://dx.doi.org/10.2514/2.7218.

Full text
APA, Harvard, Vancouver, ISO, and other styles
13

Beran, Philip, Bret Stanford, and Christopher Schrock. "Uncertainty Quantification in Aeroelasticity." Annual Review of Fluid Mechanics 49, no. 1 (January 3, 2017): 361–86. http://dx.doi.org/10.1146/annurev-fluid-122414-034441.

Full text
APA, Harvard, Vancouver, ISO, and other styles
14

Tang, D. M., and E. H. Dowell. "Nonlinear aeroelasticity in rotorcraft." Mathematical and Computer Modelling 18, no. 3-4 (August 1993): 157–84. http://dx.doi.org/10.1016/0895-7177(93)90110-k.

Full text
APA, Harvard, Vancouver, ISO, and other styles
15

Ahrem, R., A. Beckert, and H. Wendland. "Recovering rotations in aeroelasticity." Journal of Fluids and Structures 23, no. 6 (August 2007): 874–84. http://dx.doi.org/10.1016/j.jfluidstructs.2007.02.003.

Full text
APA, Harvard, Vancouver, ISO, and other styles
16

Battoo, R. S. "An introductory guide to literature in aeroelasticity." Aeronautical Journal 103, no. 1029 (November 1999): 511–18. http://dx.doi.org/10.1017/s0001924000064265.

Full text
Abstract:
AbstractThis paper is meant primarily for non-specialist readers who may not be familiar with aeroelasticity. The main objective is to direct the reader to some important texts and papers that have been published in the areas which embrace aeroelasticity, from which the reader may gain sufficient knowledge about the subject. Since aeroelasticity is a large field which requires considerable knowledge in several related areas newcomers can often be daunted by the subject. This is further compounded by the great amount of published material available. This paper will assist the reader to locate key publications and help identify major works which have been useful in studying the subject. A comprehensive list of references is included which will help to identify key subject areas, researchers, research establishments and publications for further study.
APA, Harvard, Vancouver, ISO, and other styles
17

Kasem, M. M. "Analysis, control, and optimization of aeroelastic systems: an introduction to the recent literature for the new investigator." Journal of Physics: Conference Series 2299, no. 1 (July 1, 2022): 012005. http://dx.doi.org/10.1088/1742-6596/2299/1/012005.

Full text
Abstract:
Abstract Aeroelasticity studies the static and dynamic interaction between structural deformation and fluid forces. As a result, the aeroelasticity is usually divided into three parts: aerodynamics, structural response, and dynamics with statics as a special case. Instabilities may occur to this interaction (feedback) that lead to structural failure and, even when no instability occurs, the interaction may lead to degradation or improvement of the system performance. There are several unstable phenomena may occur for elastic bodies such as flutter, divergence, low cycle oscillation, buffet, and control surface reversal. These unstable phenomena can be classified as dynamic or static. The present work provides a tutorial for those newly encountering aeroelasticity and a review of the recent literature from this century (after 2000). This includes mathematical modelling and its applications to airplanes, rotor blades, energy harvesting, and the control, and optimization of aeroelastic systems. Recent research advances are summarized and some suggestions for future work are made.
APA, Harvard, Vancouver, ISO, and other styles
18

Livne, Eli. "The Future of Airplane Aeroelasticity." Journal of Aircraft 40, no. 6 (November 2003): 1066–92. http://dx.doi.org/10.2514/1.3418.

Full text
APA, Harvard, Vancouver, ISO, and other styles
19

Bhatia, Kumar G. "Airplane Aeroelasticity: Practice and Potential." Journal of Aircraft 40, no. 6 (November 2003): 1010–18. http://dx.doi.org/10.2514/1.342.

Full text
APA, Harvard, Vancouver, ISO, and other styles
20

Dowell, Earl H., and Deman Tang. "Nonlinear Aeroelasticity and Unsteady Aerodynamics." AIAA Journal 40, no. 9 (September 2002): 1697–707. http://dx.doi.org/10.2514/2.1853.

Full text
APA, Harvard, Vancouver, ISO, and other styles
21

Schuster, David M., D. D. Liu, and Lawerence J. Huttsell. "Computational Aeroelasticity: Success, Progress, Challenge." Journal of Aircraft 40, no. 5 (September 2003): 843–56. http://dx.doi.org/10.2514/2.6875.

Full text
APA, Harvard, Vancouver, ISO, and other styles
22

Bhatia, Kumar G. "Airplane Aeroelasticity: Practice and Potential." Journal of Aircraft 40, no. 6 (November 2003): 1010–18. http://dx.doi.org/10.2514/2.7210.

Full text
APA, Harvard, Vancouver, ISO, and other styles
23

Scanlan, Robert H. "Observations on Low-Speed Aeroelasticity." Journal of Engineering Mechanics 128, no. 12 (December 2002): 1254–58. http://dx.doi.org/10.1061/(asce)0733-9399(2002)128:12(1254).

Full text
APA, Harvard, Vancouver, ISO, and other styles
24

Bendiksen, O. O. "Modern developments in computational aeroelasticity." Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 218, no. 3 (March 2004): 157–77. http://dx.doi.org/10.1243/0954410041872861.

Full text
APA, Harvard, Vancouver, ISO, and other styles
25

DOWELL, Earl H. "Unsteady transonic aerodynamics and aeroelasticity." Journal of the Japan Society for Aeronautical and Space Sciences 33, no. 383 (1985): 679–88. http://dx.doi.org/10.2322/jjsass1969.33.679.

Full text
APA, Harvard, Vancouver, ISO, and other styles
26

Dowell, Earl H. "Unsteady Transonic Aerodynamics and Aeroelasticity." Applied Mechanics Reviews 41, no. 8 (August 1, 1988): 299–319. http://dx.doi.org/10.1115/1.3151909.

Full text
Abstract:
In recent years substantial progress has been made in the development of an improved understanding of unsteady aerodynamics and aeroelasticity in the transonic flow regime. This flow regime is often the most critical for aeroelastic phenomena; yet it has proven the most difficult to master in terms of basic understanding of physical phenomena and the development of predictive mathematical models. The difficulty is primarily a result of the nonlinearities which may be important in transonic flow. Emerging mathematical models have relied principally on finite difference solutions to the governing nonlinear partial differential equations of fluid mechanics. Here are addressed fundamental questions of current interest which will provide the reader with a basis for understanding the recent and current literature in the field. Four principal questions are discussed: (1) Under what conditions are the aerodynamic forces essentially linear functions of the airfoil motion? (2) Are there viable alternative methods to finite difference procedures for solving the relevant fluid dynamical equations? (3) Under conditions when the aerodynamic forces are nonlinear functions of the airfoil motion, what is the significance of the multiple (nonunique) solutions which are sometimes observed? (4) What are effective, efficient computational procedures for using unsteady transonic aerodynamic computer codes in aeroelastic (e.g., flutter) analyses?
APA, Harvard, Vancouver, ISO, and other styles
27

Sundresan, M., D. Raja Joseph, R. Karthick, and J. C. Sherlin Shibi Joe. "Review of Aeroelasticity Testing Technology." Procedia Engineering 38 (2012): 2297–311. http://dx.doi.org/10.1016/j.proeng.2012.06.276.

Full text
APA, Harvard, Vancouver, ISO, and other styles
28

Dowell, E. H., and D. Tang. "Nonlinear aeroelasticity and unsteady aerodynamics." AIAA Journal 40 (January 2002): 1697–707. http://dx.doi.org/10.2514/3.15251.

Full text
APA, Harvard, Vancouver, ISO, and other styles
29

Dumitrache, Alexandru, and Ruxandra Botez. "Active control laws for aeroelasticity." PAMM 5, no. 1 (December 2005): 651–52. http://dx.doi.org/10.1002/pamm.200510302.

Full text
APA, Harvard, Vancouver, ISO, and other styles
30

Done, G. T. S. "Past and future progress in fixed and rotary wing aeroelasticity." Aeronautical Journal 100, no. 997 (September 1996): 269–80. http://dx.doi.org/10.1017/s0001924000028906.

Full text
Abstract:
AbstractProgress in aeroelasticity of fixed and rotary wing aircraft is compared by means of a selective review. Discussion of the role of concurrent engineering leads into modelling and validation, these being dealt with under the headings of aerodynamics, structural and integrated models. Formulation and solution of equations of motion are considered, which relate mainly to rotorcraft, and then aeroelastic performance improvement is covered. This includes optimisation, aeroservoelasticity and passive devices. Basic insight providing models are reviewed and the paper concludes with, further comments on insight, and also future progress in aeroelasticity.
APA, Harvard, Vancouver, ISO, and other styles
31

Gea, Lie-Mine, Chuen-Yen Chow, and I.-Chung Chang. "Transonic aeroelasticity analysis for rotor blades." Journal of Aircraft 29, no. 3 (May 1992): 477–84. http://dx.doi.org/10.2514/3.46186.

Full text
APA, Harvard, Vancouver, ISO, and other styles
32

Byun, Chansup, and Guru P. Guruswamy. "Wing-body aeroelasticity on parallel computers." Journal of Aircraft 33, no. 2 (March 1996): 421–28. http://dx.doi.org/10.2514/3.46954.

Full text
APA, Harvard, Vancouver, ISO, and other styles
33

Tiomkin, Sonya, and Daniella E. Raveh. "A review of membrane-wing aeroelasticity." Progress in Aerospace Sciences 126 (October 2021): 100738. http://dx.doi.org/10.1016/j.paerosci.2021.100738.

Full text
APA, Harvard, Vancouver, ISO, and other styles
34

Yu, Kok Hwa. "ACOUSTIC EFFECTS ON BINARY AEROELASTICITY MODEL." IIUM Engineering Journal 12, no. 2 (October 18, 2011): 123–30. http://dx.doi.org/10.31436/iiumej.v12i2.108.

Full text
Abstract:
Acoustics is the science concerned with the study of sound. The effects of sound on structures attract overwhelm interests and numerous studies were carried out in this particular area. Many of the preliminary investigations show that acoustic pressure produces significant influences on structures such as thin plate, membrane and also high-impedance medium like water (and other similar fluids). Thus, it is useful to investigate the structure response with the presence of acoustics on aircraft, especially on aircraft wings, tails and control surfaces which are vulnerable to flutter phenomena. The present paper describes the modeling of structural-acoustic interactions to simulate the external acoustic effect on binary flutter model. Here, the binary flutter model which illustrated as a rectangular wing is constructed using strip theory with simplified unsteady aerodynamics involving flap and pitch degree of freedom terms. The external acoustic excitation, on the other hand, is modeled using four-node quadrilateral isoparametric element via finite element approach. Both equations then carefully coupled and solved using eigenvalue solution. The mentioned approach is implemented in MATLAB and the outcome of the simulated result are later described, analyzed and illustrated in this paper.
APA, Harvard, Vancouver, ISO, and other styles
35

Cizmas, Paul G. A., Joaquin I. Gargoloff, Thomas W. Strganac, and Philip S. Beran. "Parallel Multigrid Algorithm for Aeroelasticity Simulations." Journal of Aircraft 47, no. 1 (January 2010): 53–63. http://dx.doi.org/10.2514/1.40201.

Full text
APA, Harvard, Vancouver, ISO, and other styles
36

Friedmann, Peretz P. "Renaissance of Aeroelasticity and Its Future." Journal of Aircraft 36, no. 1 (January 1999): 105–21. http://dx.doi.org/10.2514/2.2418.

Full text
APA, Harvard, Vancouver, ISO, and other styles
37

Pons, Arion, and Stefanie Gutschmidt. "Nonlinear Multiparameter Eigenvalue Problems in Aeroelasticity." International Journal of Structural Stability and Dynamics 19, no. 05 (May 2019): 1941008. http://dx.doi.org/10.1142/s0219455419410086.

Full text
Abstract:
In this work, we devise solution algorithms for nonlinear multiparameter eigenvalue problems arising in the analysis of aeroelastic flutter. Two iterative algorithms are devised, as well as a restriction method for simplifying the system behavior away from the desired flutter points. The algorithms are tested on a sectional model and on the Goland wing. Both are found to have fast and reliable convergence properties, yielding flutter point solutions which are validated by the literature. The definition of the eigenvalues is found to have a significant influence on the convergence properties of the algorithm; preferable choices for eigenvalue definitions are noted. The computational costs of the algorithms are tested and discussed; they are found to be favorable relative to other approaches from the literature. Opportunities for extending these methods are also tested and discussed.
APA, Harvard, Vancouver, ISO, and other styles
38

Hodges, Dewey H. "Review of "Theoretical and Computational Aeroelasticity"." AIAA Journal 50, no. 4 (April 2012): 990–91. http://dx.doi.org/10.2514/1.j051738.

Full text
APA, Harvard, Vancouver, ISO, and other styles
39

Friedmann, Peretz P., and Dewey H. Hodges. "Rotary Wing Aeroelasticity-A Historical Perspective." Journal of Aircraft 40, no. 6 (November 2003): 1019–46. http://dx.doi.org/10.2514/2.7216.

Full text
APA, Harvard, Vancouver, ISO, and other styles
40

Cinnella, P., P. De Palma, G. Pascazio, and M. Napolitano. "A Numerical Method for Turbomachinery Aeroelasticity." Journal of Turbomachinery 126, no. 2 (April 1, 2004): 310–16. http://dx.doi.org/10.1115/1.1738122.

Full text
Abstract:
This work provides an accurate and efficient numerical method for turbomachinery flutter. The unsteady Euler or Reynolds-averaged Navier-Stokes equations are solved in integral form, the blade passages being discretised using a background fixed C-grid and a body-fitted C-grid moving with the blade. In the overlapping region data are exchanged between the two grids at every time step, using bilinear interpolation. The method employs Roe’s second-order-accurate flux difference splitting scheme for the inviscid fluxes, a standard second-order discretisation of the viscous terms, and a three-level backward difference formula for the time derivatives. The dual-time-stepping technique is used to evaluate the nonlinear residual at each time step. The state-of-the-art second-order accuracy of unsteady transonic flow solvers is thus carried over to flutter computations. The code is proven to be accurate and efficient by computing the 4th Aeroelastic Standard Configuration, namely, the subsonic flow through a turbine cascade with flutter instability in the first bending mode, where viscous effect are found practically negligible. Then, for the very severe 11th Aeroelastic Standard Configuration, namely, transonic flow through a turbine cascade at off-design conditions, benchmark solutions are provided for various values of the inter-blade phase angle.
APA, Harvard, Vancouver, ISO, and other styles
41

Friedmann, Peretz P., and Dewey H. Hodges. "Rotary Wing Aeroelasticity-A Historical Perspective." Journal of Aircraft 40, no. 6 (November 2003): 1019–46. http://dx.doi.org/10.2514/1.2184.

Full text
APA, Harvard, Vancouver, ISO, and other styles
42

Balakrishnan, A. V. "Nonlinear Aeroelasticity: The Steady State Theory." AIAA Journal 46, no. 1 (January 2008): 177–84. http://dx.doi.org/10.2514/1.30020.

Full text
APA, Harvard, Vancouver, ISO, and other styles
43

Hodges, DH, GA Pierce, and MA Cutchins. "Introduction to Structural Dynamics and Aeroelasticity." Applied Mechanics Reviews 56, no. 3 (2003): B35. http://dx.doi.org/10.1115/1.1566393.

Full text
APA, Harvard, Vancouver, ISO, and other styles
44

Ajaj, Rafic M., and Michael I. Friswell. "Aeroelasticity of compliant span morphing wings." Smart Materials and Structures 27, no. 10 (September 21, 2018): 105052. http://dx.doi.org/10.1088/1361-665x/aad219.

Full text
APA, Harvard, Vancouver, ISO, and other styles
45

Lee, B. H. K., L. Gong, and Y. S. Wong. "Effects of structural nonlinearities in aeroelasticity." Nonlinear Analysis: Theory, Methods & Applications 30, no. 5 (December 1997): 2699–709. http://dx.doi.org/10.1016/s0362-546x(97)00338-6.

Full text
APA, Harvard, Vancouver, ISO, and other styles
46

Balakrishnan, A. V. "Possio Integral Equation of Aeroelasticity Theory." Journal of Aerospace Engineering 16, no. 4 (October 2003): 139–54. http://dx.doi.org/10.1061/(asce)0893-1321(2003)16:4(139).

Full text
APA, Harvard, Vancouver, ISO, and other styles
47

MER, K., and B. NKONGA. "Implicit Calculations of an Aeroelasticity Problem." International Journal of Computational Fluid Dynamics 9, no. 2 (March 1998): 165–78. http://dx.doi.org/10.1080/10618569808940849.

Full text
APA, Harvard, Vancouver, ISO, and other styles
48

Ringertz, U. T. "On structural optimization with aeroelasticity constraints." Structural Optimization 8, no. 1 (August 1994): 16–23. http://dx.doi.org/10.1007/bf01742928.

Full text
APA, Harvard, Vancouver, ISO, and other styles
49

Kumarasena, T., Robert H. Scanlan, and Fazl Ehsan. "Recent observations in bridge deck aeroelasticity." Journal of Wind Engineering and Industrial Aerodynamics 40, no. 3 (1992): 225–47. http://dx.doi.org/10.1016/0167-6105(92)90377-m.

Full text
APA, Harvard, Vancouver, ISO, and other styles
50

Matsumoto, Masaru, and Yukio Tamura. "Survey for the aeroelasticity of structures." Journal of Wind Engineering and Industrial Aerodynamics 46-47 (August 1993): 873–77. http://dx.doi.org/10.1016/0167-6105(93)90366-v.

Full text
APA, Harvard, Vancouver, ISO, and other styles
You might also be interested in the bibliographies on the topic 'Aeroelasticity' for other source types:
Dissertations / Theses Books
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography