Experimental Study of Aeroelastic Response and Performance of a Hypersonic Intake Ramp
Author:
Affiliation:
1. University of New South Wales, Canberra, Australian Capital Territory 2612, Australia
2. University of Southern Queensland, Toowoomba, Queensland 4350, Australia
Funder
Air Force Office of Scientific Research
National Computational Infrastructure
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B38348
Reference28 articles.
1. Coupled thermal, structural and vibrational analysis of a hypersonic engine for flight test
2. KlineH. L.PalaciosF.AlonsoJ. J. “Sensitivity of the Performance of a 3-Dimensional Hypersonic Inlet to Shape Deformations,” AIAA Paper 2014-3228, June 2014. 10.2514/6.2014-3228
3. GuangyueD.ZengL.JiaH.LiuL.QiuB.GuiY. “Preliminary Study on the Influence of Aerothermoelastic Deformation on 2-D Hypersonic Inlet Performance,” AIAA Paper 2017-2403, March 2017. 10.2514/6.2017-2403
4. Effects of the aerothermoelastic deformation on the performance of the three-dimensional hypersonic inlet
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