Effect of engine integration on the aerodynamic characteristics of a spaceplane

International Journal of Computational Fluid Dynamics

Volumn 8, Issue 4, 1997, Pages 235-246

  Fujii, K ^a   Tamura, Y ^a  

^a JAPAN AEROSPACE EXPLORATION AGENCY   (Japan)

Author keywords

Navier Stokes simulations; Spaceplane; Supersonic flows; Zonal method

Indexed keywords

EID: 0031314314     PISSN: 10618562     EISSN: None     Source Type: Journal    
DOI: 10.1080/10618569708940806     Document Type: Article

References (12)

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3. Sakata, K., Honami, S. and Tanaka, A. (1991). "Supersonic Airintake Study Aiming at Future Airbreathing Engine," AIAA Paper 91-2012, June.
4. Kuroda, S. and Fujii, K. (1991). "Supersonic Inlet Flow Computations Using Fortified Navier-Stokes Approach", AIAA Paper 91-1730, June.
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6. Kuroda, S. (1993). "Numerical Simulation of Supersonic Flow around Space Plane for Airframe-Engine Integration," AIAA Paper 93-0886, Jan.
7. Fujii, K. and Tamura, Y. (1995). "Effect of the Engine Integration to the Aerodynamic Characteristics of a Spaceplane," Preprint of the 6th International Symposium on Computational Fluid Dynamics -lake Tahoe, September, pp. 341-346.
8. Shang, J. S. (1985). "Navier-Stokes Solution of the Flow Field around a Complete Aircraft," AIAA Paper 85-509.
9. Richardson, P., Parletter, E., Morrison, J., Switzer, G, Dilley, A. and Eppard, W. (1989). "Heat Transfer and Pressure Comparisons between Computation and Wind Tunnel for a Research Hypersonic Aircraft," AIAA Paper 89-0029.
10. Chen, C. L., Ramakrishnan, S., Szema, K.Y., Dresser, H. S. and Rajagopal, K. (1992). "Multizonal Navier-Stokes Solutions for the Multibody Space Shuttle Configuration," Journal of Spacecraft and Rockets, 29(1).
11. Fujii, K. (1995). "Unified Zonal Method Based on the Fortified Solution Algorithm," Journal of Computational Physics, 118, pp. 92-108.
12. Fujii, K. (1989). "High-Resolution Upwind Scheme for Vortical-Flow Simulations," Journal of Aircraft, 26(12), pp. 1123-1129.