Author:
Liu Jin,Song Yuhui,Hu Jing
Reference12 articles.
1. Liu J, Chen N, Song Y et al (2015) New dynamic stability rig for tri-sonic wind-tunnel. Procedia Eng 99:1591–1596
2. McClinton CR, Holland SD, Rock KE et al (1998) Hyper-X wind tunnel program. In: AIAA-1998-0553. AIAA, Reno
3. Holland SD, Woods WC, Engelund WC (2000) Hyper-X Research Vehicle (HXRV) experimental aerodynamics test program overview. In: AIAA-2000-4011. AIAA, Denver
4. Boyden RP, Freeman DC Jr (1976) Subsonic and transonic dynamic stability characteristics of a space shuttle orbiter. In: NASA-TN-D-8042. NASA, Hampton
5. Penland JA, Dillon JL, Pittman JL (1978) An aerodynamic analysis of several hypersonic research airplane concepts from M = 0.2 to 6.0. In: AIAA-78-150. AIAA, Huntsville