Optimization of two-dimensional scramjet inlets

Journal of Aircraft

Volumn 36, Issue 2, 1999, Pages 430-433

  Smart, M K ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

JET AIRCRAFT; LAGRANGE MULTIPLIERS; OPTIMIZATION; SHOCK WAVES; SUPERSONIC AERODYNAMICS;

SUPERSONIC INLETS;

INTAKE SYSTEMS;

EID: 0032626772     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.2448     Document Type: Article

References (4)

1. Oswatitsch, K., "Pressure Recovery for Missiles with Reaction Propulsion at High Supersonic Speeds (the Efficiency of Shock Diffusers)," NACA TM 1140 (translation), 1947.
2. Hermann, R., Supersonic Inlet Diffusers and Introduction to Internal Aerodynamics, Honeywell Regulator Co., Minneapolis, MN, 1956, p. 171, Chap. 5.
3. Sokolnikoff, I., Advanced Calculus, McGraw-Hill, New York, 1939, p. 332.
4. Press, W. H., Teukolsky, S. A., Vetterling, W. T., and Flannery, B. P., Numerical Recipes in Fortran, 2nd ed., Cambridge Univ. Press, New York, 1992, p. 382, Chap. 9.