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Статті в журналах з теми "Aerospace measurements"
Kingsley-Rowe, J. R., G. D. Lock, and A. G. Davies. "Aerospace applications of luminescent paint." Aeronautical Journal 107, no. 1077 (November 2003): 637–48. http://dx.doi.org/10.1017/s0001924000013518.
Повний текст джерелаKingsley-Rowe, J. R., G. D. Lock, and A. G. Davies. "Aerospace applications of luminescent paint." Aeronautical Journal 107, no. 1077 (November 2003): 649–56. http://dx.doi.org/10.1017/s000192400001352x.
Повний текст джерелаKondratyev, K. Ya, V. V. Kozoderov, and P. P. Fedchenko. "Studies of vegetation and soils from aerospace measurements." Advances in Space Research 5, no. 6 (January 1985): 355–57. http://dx.doi.org/10.1016/0273-1177(85)90341-2.
Повний текст джерелаPongsakornsathien, Nichakorn, Alessandro Gardi, Yixiang Lim, Roberto Sabatini, and Trevor Kistan. "Wearable Cardiorespiratory Sensors for Aerospace Applications." Sensors 22, no. 13 (June 21, 2022): 4673. http://dx.doi.org/10.3390/s22134673.
Повний текст джерелаOrnat, Artur, Marek Uliasz, Grzegorz Bomba, Andrzej Burghardt, Krzysztof Kurc, and Dariusz Szybicki. "Robotised Geometric Inspection of Thin-Walled Aerospace Casings." Sensors 22, no. 9 (May 1, 2022): 3457. http://dx.doi.org/10.3390/s22093457.
Повний текст джерелаHajiyev, Chingiz, and Ahmet Sofyali. "Spacecraft localization by indirect linear measurements from a single antenna." Aircraft Engineering and Aerospace Technology 90, no. 5 (July 2, 2018): 734–42. http://dx.doi.org/10.1108/aeat-12-2015-0245.
Повний текст джерелаBerri, Pier Carlo, Matteo D. L. Dalla Vedova, and Paolo Maggiore. "Experimental comparison of Fiber Bragg Grating installation techniques for aerospace systems." MATEC Web of Conferences 304 (2019): 04012. http://dx.doi.org/10.1051/matecconf/201930404012.
Повний текст джерелаMagdziak, Marek. "The influence of a number of points on results of measurements of a turbine blade." Aircraft Engineering and Aerospace Technology 89, no. 6 (October 2, 2017): 953–59. http://dx.doi.org/10.1108/aeat-03-2016-0044.
Повний текст джерелаJansson, N., and G. Stenfelt. "Steady and unsteady pressure measurements on a swept-wing aircraft." Aeronautical Journal 118, no. 1200 (February 2014): 109–22. http://dx.doi.org/10.1017/s0001924000009015.
Повний текст джерелаKing, Andrew, A. D. Evans, Philip J. Withers, and C. Woodward. "The Effect of Fatigue on Residual Peening Stresses in Aerospace Components." Materials Science Forum 490-491 (July 2005): 340–45. http://dx.doi.org/10.4028/www.scientific.net/msf.490-491.340.
Повний текст джерелаДисертації з теми "Aerospace measurements"
Husen, Nicholas M. "Skin Friction Measurements Using Luminescent Oil Films." Thesis, Purdue University, 2017. http://pqdtopen.proquest.com/#viewpdf?dispub=10277794.
Повний текст джерелаAs aircraft are designed to a greater extent on computers, the need for accurate and fast CFD algorithms has never been greater. The development of CFD algorithms requires experimental data against which CFD output can be validated and from which insight about flow physics can be acquired. Skin friction, in particular, is an important quantity to predict with CFD, and experimental skin friction data sets aid not only with the validation of the CFD predictions, but also in tuning the CFD models to predict specific flow fields. However, a practical experimental technique for collecting spatially and temporally resolved skin friction data on complex models does not yet exist. This dissertation develops and demonstrates a new luminescent oil film skin friction meter which can produce spatially-resolved quantitative steady and unsteady skin friction data on models with complex curvature.
The skin friction acting on the surface of a thin film of oil can be approximated by the expression τw =μ ouh/h, where μ o is the dynamic viscosity of the oil, uh is the velocity of the surface of the oil film, and h is the thickness of the oil film. The new skin friction meter determines skin friction by measuring h and uh. The oil film thickness h is determined by ratioing the intensity of the fluorescent emissions from the oil film with the intensity of the incident light which is scattered from the surface of the model. When properly calibrated, that ratio provides an absolute oil film thickness value. This oil film thickness meter is therefore referred as the Ratioed-Image Film-Thickness (RIFT) Meter. The oil film velocity uh is determined by monitoring the evolution of tagged molecules within the oil film: Photochromic molecules are dissolved into the fluorescent oil and a pattern is written into the oil film using an ultraviolet laser. The evolution of the pattern is recorded, and standard cross-correlation techniques are applied to the resulting sequence of images. This newly developed skin friction meter is therefore called the Luminescent Oil Film Flow-Tagging skin friction meter, or the LOFFT skin friction meter. The LOFFT skin friction meter is demonstrated by collecting time-averaged skin friction measurements on NASA's FAITH model and by collecting unsteady skin friction measurements with a frequency response of 600Hz. Higher frequency response is possible and is dependent on the experimental setup.
This dissertation also contributes to the work done on the Global Luminescent Oil Film Skin Friction Meter (GLOFSFM) by noting that the technique could be influenced by ripples at the oil-air interface. An experiment studying the evolution of ripples at the oil-air interface was conducted to determine under what oil film conditions the GLOFSFM can be appropriately applied. The RIFT meter was crucial for this experiment, as it facilitated quantitative distributed oil film thickness measurements during the wind-tunnel run. The resulting data set is rich in content, permitting the computation of mean wavelengths, peak-to-trough ripple heights, wave speeds, and mean thicknesses. In addition to determining under what oil film conditions the GLOFSFM may be applied, this experiment directly determined the oil film conditions under which the velocity of the ripples may be used to proxy the velocity of the oil film surface. The RIFT meter and the ability to determine oil film surface velocity by monitoring ripple velocities admit yet another time-averaged skin friction meter, the Fluorescent-Oil Ripple-Velocity (FORV) skin friction meter. The FORV skin friction meter recovers skin friction as τ w = μovrip/H, where vrip is the velocity of the ripples, and H is the oil film thickness averaged over the thickness fluctuations due to the ripples. The FORV skin friction meter is demonstrated on NASA's FAITH model.
Levedahl, Blaine Alexander. "Vehicle Control in Full Unsteady Flow Using Surface Measurements." NCSU, 2010. http://www.lib.ncsu.edu/theses/available/etd-02272010-190048/.
Повний текст джерелаJohnson, Peder. "Dua-beam digital speckle photography : strain field measurements in aerospace applications." Licentiate thesis, Luleå tekniska universitet, 1998. http://urn.kb.se/resolve?urn=urn:nbn:se:ltu:diva-26085.
Повний текст джерелаPrice, Jennifer Lou. "Unsteady Measurements and Computations on an Oscillating Airfoil with Gurney Flaps." NCSU, 2001. http://www.lib.ncsu.edu/theses/available/etd-20010713-170959.
Повний текст джерелаPrice, Jennifer Lou. Unsteady Measurements and Computations on an Oscillating Airfoil with Gurney Flaps. (Under the direction of Dr. Ndaona Chokani)The effect of a Gurney flap on an unsteady airfoil flow is experimentally and computationally examined. In the experiment, the details of the unsteady boundary layer events on the forward portion of the airfoil are measured. In the computation, the features of the global unsteady flow are documented and correlated with the experimental observations.The experiments were conducted in the North Carolina State University subsonic wind tunnel on an oscillating airfoil at pitch rates of 65.45 degrees/sec and 130.9 degrees/sec. The airfoil has a NACA0012 cross-section and is equipped with a 1.5% or 2.5% chord Gurney flap. The airfoil is tested at Reynolds numbers of 96,000, 169,000 and 192,000 for attached and light dynamic stall conditions. An array of surface-mounted hot-film sensors on the forward 25% chord of the airfoil is used to measure the unsteady laminar boundary layer separation, transition-to-turbulence, and turbulent reattachment. In parallel with the experiments incompressible Navier-Stokes computations are conducted for the light dynamic stall conditions on the airfoil with a 2.5%c Gurney flap at a Reynolds number of 169,000.The experimental measurements show that the effect of the Gurney flap is to move the separation, transition and reattachment forward on the airfoil. This effect is more marked during the airfoil's pitch-down than during pitch-up. The computational results verify these observations, and also show that the shedding of the dynamic stall vortex is delayed. Thus the adverse effects of dynamic stall are mitigated by the Gurney flap.
Jones, Warren Anthony. "CONTROL OF DIFFUSING DUCT FLOWUSING ACTIVE VORTEX GENERATORSWITH HOT-FILM SENSOR MEASUREMENTS." NCSU, 2001. http://www.lib.ncsu.edu/theses/available/etd-20010528-224402.
Повний текст джерелаExperiments have been conducted using vane-type vortex generators to control flow separation and exit flow distortion in a diffusing duct. The primary purpose is to examine the feasibility of using surface-mounted hot-film sensors to determine the extent of exit flow distortion. The experimental set-up consists of a two-dimensional blow down type wind tunnel with a variable diffuser exit. One diffuser wall is curved to produce a Stratford-like pressure gradient. The wall's placement is adjustable such that the adverse pressure gradient can be adjusted to promote separation. An active vortex generator array that can be placed at three streamwise locations is used to reduce the extent of flow separation and exit distortion.Diffuser surface pressure and exit total pressure measurements are obtained and compared to the hot-film data. The time-averaged mean and rms voltages from the hot-film data are used as indicators of flow separation and exit flow distortion.Results show that, with the use of the vortex generators, high mean voltages and low levels of rms voltage correlate well with improved pressure recovery. Conversely, poorer pressure recovery is associated with lower mean voltages and higher rms values compared to the baseline cases. Increased total pressures at the diffuser exit are accompanied by increases in hot-film mean voltages. These indicate higher shear stresses, which also correspond to increased flow uniformity. Lower variations in the rms voltages compared to the baseline cases also correlated well with improved total pressures at the diffuser exit.
Tedder, Sarah Augusta. "Advancements in dual-pump broadband CARS for supersonic combustion measurements." W&M ScholarWorks, 2010. https://scholarworks.wm.edu/etd/1539623572.
Повний текст джерелаPool, Kirby Vinton. "Product/process improvement through performance measurements and modeling : a case study in aerospace welding." Thesis, Massachusetts Institute of Technology, 1991. http://hdl.handle.net/1721.1/13376.
Повний текст джерелаIncludes bibliographical references (leaves 135-136).
by Kirby Vinton Pool.
M.S.
Bifano, Michael F. P. "Theory and Measurements of Thermal Properties in Nanowires and Carbon Nanotubes." Case Western Reserve University School of Graduate Studies / OhioLINK, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=case1339998535.
Повний текст джерелаBrewer, David A. "Plume Contamination Measurements of an Additively-Printed GOX/ABS Hybrid Thruster." DigitalCommons@USU, 2018. https://digitalcommons.usu.edu/etd/7072.
Повний текст джерелаBarone, Dominic L. "Investigation of TDLAS Measurements in a Scramjet Engine." University of Cincinnati / OhioLINK, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1277130335.
Повний текст джерелаКниги з теми "Aerospace measurements"
Ehernberger, L. J. Stratospheric turbulence measurements and models for aerospace plane design. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1992.
Знайти повний текст джерелаVisentine, James T. Material interactions with the low earth orbital environment: Accurate reaction rate measurements. New York: AIAA, 1986.
Знайти повний текст джерелаVisentine, James T. Atomic oxygen effects measurements for shuttle missions STS-8 and 41-G. Washington, D. C: Lyndon B. Johnson Space Center, 1988.
Знайти повний текст джерелаRogers, Melissa J. B. Summary report of mission acceleration measurements for STS-73, launched October 20, 1995. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаShen kong ce kong wu xian dian ce liang ji shu: Radiometric measuring techniques for deep space navigation. Beijing Shi: Guo fang gong ye chu ban she, 2012.
Знайти повний текст джерелаBenton, E. V. Environmental radiation measurements on MIR station: Program 1--internal experiment, program 2--external experiment : year 2 progress report, contract no. NCC2-893. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаRogers, Melissa J. B. Summary report of mission acceleration measurements for STS-60, SPACEHAB-2 launched February 11, 1994. Cleveland, Ohio: NASA Lewis Research Center, 1994.
Знайти повний текст джерелаNoyes, Gerold. Performance measurements and energy balance of an SPS V160 Stirling motor at the German Aerospace Research Establishment. Köln: Deutsche Forschungsanstalt für Luft- und Raumfahrt, 1990.
Знайти повний текст джерелаInternational Congress on Instrumentation in Aerospace Simulation Facilities (19th 2001 Cleveland, Ohio). ICIASF '01: 19th International Congress on Instrumentation in Aerospace Simulation Facilities, Leveraging resources through collaboration, 22800 Cedar Point Road, Cleveland, Ohio 44142, August 27-30, 2001. Piscataway, N.J: IEEE Service Center, 2001.
Знайти повний текст джерелаShen kong ce kong tong xin xi tong gong cheng yu ji shu: Engineering and Technology of Deep Space TT&C System. Beijing Shi: Ke xue chu ban she, 2013.
Знайти повний текст джерелаЧастини книг з теми "Aerospace measurements"
Boden, Fritz, Thomas Wolf, Claudio Lanari, and Anwar Torres. "IPCT Ground Vibration Measurements on a Small Aircraft." In Research Topics in Aerospace, 33–55. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_4.
Повний текст джерелаKindler, Kolja, Karen Mulleners, and Markus Raffel. "Towards In-Flight Measurements of Helicopter Blade Tip Vortices." In Research Topics in Aerospace, 171–85. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_11.
Повний текст джерелаBoden, Fritz, Henk Jentink, and Christian Petit. "IPCT Wing Deformation Measurements on a Large Transport Aircraft." In Research Topics in Aerospace, 93–115. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_7.
Повний текст джерелаBoden, Fritz, Claudio Lanari, Anwar Torres, and Thorsten Weikert. "In-Flight IPCT Wing Deformation Measurements on a Small Aircraft." In Research Topics in Aerospace, 57–72. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_5.
Повний текст джерелаRužička, Pavel, Jan Rýdel, Miroslav Josefik, and Fritz Boden. "Assessment of IPCT for Wing Deformation Measurements on Small Aircrafts." In Research Topics in Aerospace, 73–92. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_6.
Повний текст джерелаLanari, Claudio, Boleslaw Stasicki, Fritz Boden, and Anwar Torres. "Image Based Propeller Deformation Measurements on the Piaggio P 180." In Research Topics in Aerospace, 133–53. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_9.
Повний текст джерелаMaucher, Christoph, and Fritz Boden. "Blade Deformation Measurements with IPCT on an EC 135 Helicopter Rotor." In Research Topics in Aerospace, 195–213. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_13.
Повний текст джерелаVeerman, H. P. J., H. Kannemans, and H. W. Jentink. "Highly Accurate Aircraft In-Flight Wing Deformation Measurements Based on Image Correlation." In Research Topics in Aerospace, 15–32. Berlin, Heidelberg: Springer Berlin Heidelberg, 2013. http://dx.doi.org/10.1007/978-3-642-34738-2_3.
Повний текст джерелаBeswick, John M. "Chapter 17 | Super-Precision Aerospace Bearing Steel Technologies." In Rolling Bearing Steel: Design, Technology, Testing and Measurements, 313–50. 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959: ASTM International, 2022. http://dx.doi.org/10.1520/mnl8320200019.
Повний текст джерелаSanfedino, Francesco, Marco Scardino, Jérémie Chaix, and Stéphanie Lizy-Destrez. "CubeSat Attitude Estimation via AUKF Using Magnetometer Measurements and MRPs." In Advances in Aerospace Guidance, Navigation and Control, 343–61. Cham: Springer International Publishing, 2015. http://dx.doi.org/10.1007/978-3-319-17518-8_20.
Повний текст джерелаТези доповідей конференцій з теми "Aerospace measurements"
Mercer, Carolyn R. "Optical measurements for intelligent aerospace propulsion." In Optical Science and Technology, SPIE's 48th Annual Meeting, edited by Patrick V. Farrell, Fu-Pen Chiang, Carolyn R. Mercer, and Gongxin Shen. SPIE, 2003. http://dx.doi.org/10.1117/12.509732.
Повний текст джерелаTIGHE, THOMAS, and RALPH SHIMOVETZ. "SARL noise measurements." In 28th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1990. http://dx.doi.org/10.2514/6.1990-285.
Повний текст джерелаSmith, Robert W., and Ted Corbin. "LOWTRAN 7 comparisons with field measurements." In Aerospace Sensing, edited by Dieter Clement and Wendell R. Watkins. SPIE, 1992. http://dx.doi.org/10.1117/12.137849.
Повний текст джерелаNomura, Satoshi, Gen Ito, Kazuhisa Fujita, and Kimiya Komurasaki. "Translational Temperature Measurements in Shock Layer by Point-measurement Laser Absorption Spectroscopy." In 52nd Aerospace Sciences Meeting. Reston, Virginia: American Institute of Aeronautics and Astronautics, 2014. http://dx.doi.org/10.2514/6.2014-1409.
Повний текст джерелаSeichepine, Nicolas, Jerome Lacaille, and J. Ricordeau. "Data mining of flight measurements." In Infotech@Aerospace 2011. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2011. http://dx.doi.org/10.2514/6.2011-1530.
Повний текст джерелаEichelberger, H., G. Fremuth, G. Prattes, Ch Kurbisch, G. Laky, F. Giner, S. Neukirchner, et al. "BepiColombo-MPO-SERENA-PICAM EMC measurements." In 2016 ESA Workshop on Aerospace EMC (Aerospace EMC). IEEE, 2016. http://dx.doi.org/10.1109/aeroemc.2016.7504548.
Повний текст джерелаGoebel, John H., Theodore T. Weber, Arthur D. Van Rheenen, Leon L. Jostad, Joo-Young Kim, and Ben Gable. "Cryogenic measurements of Aerojet GaAs n-JFETs." In Aerospace Sensing, edited by Eric R. Fossum. SPIE, 1992. http://dx.doi.org/10.1117/12.60499.
Повний текст джерелаGrant, Michael, Stephen Katzberg, and Roland Lawrence. "GPS Remote Sensing Measurements Using Aerosonde UAV." In Infotech@Aerospace. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-7005.
Повний текст джерелаNORTON, OLIN, R. KUMAR, and D. SRIKANTAIAH. "A direct comparison of cross-correlation velocity measurements with laser Doppler measurements." In 29th Aerospace Sciences Meeting. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1991. http://dx.doi.org/10.2514/6.1991-213.
Повний текст джерелаEHERNBERGER, L. "Stratospheric turbulence measurements and models for aerospace planedesign." In AlAA 4th International Aerospace Planes Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-5072.
Повний текст джерелаЗвіти організацій з теми "Aerospace measurements"
Liou, K. N. Interpretation of Radiation Measurements from UAV. Final Report [Unmanned Aerospace Vehicles]. Office of Scientific and Technical Information (OSTI), July 2000. http://dx.doi.org/10.2172/763424.
Повний текст джерелаCalkins, Dale E., Richard S. Gaevert, Frederick J. Michel, and Karen J. Richter. Aerospace System Unified Life Cycle Engineering Producibility Measurement Issues. Fort Belvoir, VA: Defense Technical Information Center, May 1989. http://dx.doi.org/10.21236/ada210937.
Повний текст джерелаCatherine Gautier. Atmospheric radiation measurement - unmanned aerospace vehicle. Final technical report. Office of Scientific and Technical Information (OSTI), March 2000. http://dx.doi.org/10.2172/764576.
Повний текст джерелаGautier, Catherine. Final Report: Atmospheric Radiation Measurement Unmanned Aerospace Vehicle, February 1, 1995 - January 31, 1999. Office of Scientific and Technical Information (OSTI), January 1999. http://dx.doi.org/10.2172/765148.
Повний текст джерелаNoguchi, R. Environmental effects on composite airframes: A study conducted for the ARM UAV Program (Atmospheric Radiation Measurement Unmanned Aerospace Vehicle). Office of Scientific and Technical Information (OSTI), June 1994. http://dx.doi.org/10.2172/10166660.
Повний текст джерелаRoye, Thorsten. Unsettled Technology Areas in Deterministic Assembly Approaches for Industry 4.0. SAE International, August 2021. http://dx.doi.org/10.4271/epr2021018.
Повний текст джерела