Critical design issues for airbreathing hypersonic waverider missiles

Journal of Spacecraft and Rockets

Volumn 38, Issue 4, 2001, Pages 510-519

  Starkey, R P ^a   Lewis, M J ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT FUELS; COMPUTER SIMULATION; GENETIC ALGORITHMS; HYDROCARBONS; HYPERSONIC AERODYNAMICS; MACHINE DESIGN; MILITARY VEHICLES; SENSITIVITY ANALYSIS; VTOL/STOL AIRCRAFT; WORKING FLUID PRESSURE INDICATORS;

HYPERSONIC WAVERIDER MISSILES;

MISSILES;

EID: 0035389997     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3734     Document Type: Article

References (19)

1. Aerodynamic problems of manned space vehicles
2. Navier-stokes computation of a viscous optimized waverider
3. Performance study of a power law starbody
4. Simple analytical model for parameteric studies of hypersonic waveriders
5. Missile aerodynamic shape optimization using genetic algorithms
6. SHARP-L1 technology demonstrator development: An aerothermodynamic perspective
7. Experimental results on a mach 14 waverider with blunt leading edges
8. Stability and control of hypersonic waverider vehicles
9. Optimization of waverider-based hypersonic cruise vehicles with off-design considerations
10. Analytical off-design L/D analysis for hypersonic waveriders with planar shocks
11. Joint jet-A/silane/hydrogen reaction mechanism