Computational optimization of a hypersonic rectangular-to-circular inlet

Journal of Propulsion and Power

Volumn 17, Issue 3, 2001, Pages 571-578

  Sabean, J W ^a   Lewis, M J ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMBUSTORS; COMPRESSORS; COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; OPTIMIZATION;

EULER EQUATIONS; HYPERSONIC INLETS;

HYPERSONIC FLOW;

EID: 0035331028     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5779     Document Type: Article

References (11)

1. Design of three-dimensional hypersonic inlets with rectangular to elliptical shape transition
2. Automated redesign of the NASA P8 hypersonic inlet using numerical optimization
3. Optimized scramjet integration on a waverider
4. Wind-tunnel testing, flight scaling, and flight validation with hyper-X
5. Comparison of shock-induced two- and three dimensional incipient turbulent separation
6. Improving the efficiency of aerodynamic shape optimization
7. Performance study of a power law star body
8. Engine-airframe integration on osculating cone waverider-based vehicle designs