Hypersonic detonation wave powered lifting-propulsive bodies

AIAA 3rd International Aerospace Planes Conference, 1991

Volumn , Issue , 1991, Pages

  Atamanchuk, Taras M ^a   Sislian, Jean P ^a  

^a UNIVERSITY OF TORONTO   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE VEHICLES; COMBUSTION; COMPUTATIONAL GEOMETRY; DETONATION; FLOW FIELDS; SHOCK WAVES;

DESIGN CONDITION; DETONATION WAVES; FINITE REACTION RATES; HYPERSONIC PROPULSION; INTERSECTION POINTS; PERFORMANCE PARAMETERS; STOICHIOMETRIC MIXTURES; TRACKING CAPABILITY;

COMBUSTION KNOCK;

EID: 85006413296     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1991-5010     Document Type: Conference Paper

References (10)

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2. Atamanchuk, T. M., and Sislian, J. P.,“ Performance Characteristics of Hypersonic Detonation Wave Ramjets”, Proceedings of the Seventy-fifth AGARD Symposium of the Propulsion and Energetics Panel on Hypersonic Combined Cycle Propulsion. Madrid. Spain. 28 May-1 June 1990.
3. Sislian J. P. and Atamanchuk, T. M., “Aerodynamic and Propulsive Performance of Hypersonic Detonation Wave Ramjets”, Proceedings of the Ninth International Symposium on Air Breathing Engines, 1989.pp. 1026-1035.
4. Jachimowski C. J., “An Analytical Study of the Hydrogen-Air Reaction Mechanism With Application to Scramjet Combustion”, Langley Research Center, Hampton, Virginia. NASA Technical Paper 2791, 1988
5. Goduov S. K., (ed.), Numerical Solution of Multidimensional Problems of Gasdynamics. Nauka, Moscow. 1976.
6. Rodionov, A. V., “Second-Order Accurate Monotonic Scheme for Nonequilibrium Flow Computation”, Zhurnal Bycheslitelnoy Matematiki i Mathe-maticheskai Fiziki, (in Russian), 1987, 27, No.4, pp. 585-593.
7. Zucrow M. J., arid Hoffman J. D., Gas Dynamics, Vol. 1. John Wiley and Sons Inc., Toronto. 1976.
8. Townend, L. H., “On Lifting Bodies which Contain Two-Dimensional Supersonic Flows”, Royal Aircraft Establishment. Reports and Memoranda No. 3383. Aug. 1963.
9. Kuchemann, D., “Hypersonic Aircraft and Their Aerodynamic Problems”, Em Progress in Aeronautical Sciences. No. 5. Vol. 6. 1965.pp. 271-353.
10. Raymer, D. P., Aircraft Design: A Conceptual Approach, AIAA Educational Series. Washington D C.. 1989.