A study on the full flowpath and the aerodynamic characteristic of an axisymmetric hypersonic vehicle

Hangkong Dongli Xuebao/Journal of Aerospace Power

Volumn 22, Issue 6, 2007, Pages 967-973

  Sun, Shu ^a   Zhang, Hong Ying ^a   Wang, Cheng Peng ^a   Lu, Ying Wei ^a   Cheng, Ke Ming ^a   Wu, Yi Zhao ^a  

^a NANJING UNIVERSITY OF AERONAUTICS AND ASTRONAUTICS   (China)

Author keywords

Aerospace propulsion system; Axisymmetric hypersonic vehicle; Drag coefficient; Free stream Mach number; Full flowpath; Lift coefficient

Indexed keywords

AEROSPACE PROPULSION SYSTEM; AXISYMMETRIC HYPERSONIC VEHICLE; FULL FLOWPATH; LIFT COEFFICIENT;

ANGLE OF ATTACK; COMPUTATIONAL FLUID DYNAMICS; DRAG COEFFICIENT; FLOW PATTERNS; FLOW STRUCTURE; MACH NUMBER; PROPULSION; REYNOLDS NUMBER;

AERODYNAMICS;

EID: 34447343766     PISSN: 10008055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (14)

1. William H, Davis P. Hypersonic airbrcathing propulsion [M], AIAA Education Series, AIAA Inc, USA, 1994.
2. Bachchan N, Hillier R. Hypersonic inlet flow analysis at off-design conditlons [R]. AIAA 2004-5380.
3. Zanchetta M, Cain T. An axismmetric internal compression inlet [R]. AIAA 1998-7957.
4. Hsia Yeu-Chuan. Full navier-stokes analysis of an axisym-metric scramjet mlet [J]. Journal of Propulsion and Power, 1993, 9 (4): 826-833.
5. TAN Huijun, GUO Rongwei. Wind tunnel tests of hypersonic inlets for ramjet models of the ramjet-scramjet combined engine [J]. Acta Aeronautica et Astronautica Sinica, 2007, 28 (4): 686-693.
6. Smart M K. Design of three-simensional hypersonic inlets with rectangular to elliptical shape transition [J]. Journal of Propulsion and Power, 1999, 15 (3): 512-520.
7. Watanabe Y, Miyagi H, Sekido T. Conceptual design study on combine-cycle engine for hypersonic transport [R], IS-ABE-93-7018.
8. Voland R T, Auslender A H. CIAM/NASA Mach 6.5 Scramjet Flight and Ground Test [R]. AIAA 1999-4848.
9. Roudakov A S, Semenov V L. Recent flight test results of the joint CIAM-NASA Mach 6.5 scramjet flight program [R]. AIAA 1996-0357.
10. Billing F S. Shock-wave shapes around spherical- and cylindrical-nosed bodies [J]. Journal of Spacecraft and Rockets, 1967, 4 (6): 822-823.
11. Edney B E. Effects of shock impingement of the heat transfer around blunt bodies [J]. AIAA Journal, 1986, 16 (1): 15-21.
12. ZHANG Hongying. SUN Shu, CHENG Kerning, et al. Experimental investigation of inlet start/unstart influences on the aerodynamic characteristic of a hypersonic vehicle [J]. Journal of Astronautics, 2007, 28 (4): 624-628.
13. SUN Shu, ZHANG Hongying, CHENG Kerning, et al. A study of the full flowpath of a hypersonic vehicle [J]. Acta Aeronautica et Astronautica Sinica, 2007, 28 (6). 912-917.
14. Tan H J, Guo R W. Experimental study of the unstable-unstarted condition of a hypersonic inlet at Mach 6 [J]. Journal of Propulsion and Power, 2007, 23 (6): 715-726.