Supersonic Indicial Response with Nonlinear Corrections by Shock and Rarefaction Waves

Author:

Bai Chen-Yuan1,Wu Zi-Niu1

Affiliation:

1. Tsinghua University, 100084 Beijing, People’s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Reference29 articles.

1. AndersonJ. D., Introduction to Flight, McGraw-Hill Higher Education, Boston, 2000, pp. 467–526, Chap. 7.

2. BisplinghoffR. L.AshleyH.HalfmanR. L., Aeroelasticity, Addison–Wesley, Reading, MA, 1995, pp. 294–375, Chap. 6.

3. HeasletM. A.LomaxH. “Two-Dimensional Unsteady Lift ProbIems in Supersonic FIight,” Archive and Image Library TR 945, Washington, D.C. 1949;

4. Loads on a Supersonic Wing Striking a Sharp-Edged Gust

5. Linearized Aeroelastic Gust Response Analysis of a Launch Vehicle

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