Significance of fuel selection for hypersonic vehicle range

Journal of Propulsion and Power

Volumn 17, Issue 6, 2001, Pages 1214-1221

  Lewis, M J ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DENSITY (SPECIFIC GRAVITY); DRAG; FLIGHT DYNAMICS; HYDROCARBONS; HYDROGEN FUELS; HYPERSONIC AERODYNAMICS; LIFT; LIQUID FUELS; PERFORMANCE;

HYPERSONIC AIRCRAFT; HYPERSONIC FLIGHT; LIFT-OVER-DRAG RATIO;

AIRCRAFT FUELS;

EID: 0035510634     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5866     Document Type: Article

References (25)

1. Survey of jet fuels (1990-1996)
2. Surrogate mixtures to represent complex aviation and rocket fuels
3. Gas turbine fuels
4. Hydrocarbon fuel cooling technologies for advanced propulsion
5. New directions in hypersonic technologies
6. Optimized scramjet integration on a waverider
7. Design tradeoffs on scramjet engine integrated hypersonic waverider vehicles
8. Periodic optimal flight
9. Energy state approximation in performance optimization of supersonic aircraft
10. Analysis of experimental results on a Mach 14 waverider with blunt leading edges
11. Prediction of range and endurance of jet aircraft at constant altitude
12. Some readily quantifiable aspects of scramjet engine performance
13. Optimization of waverider-based cruise vehicles with off-design considerations
14. Waverider configuration development for the dual fuel vehicle
15. Simple analytical model for parametric studies of hypersonic waveriders
16. Watts - a computer program for weights analysis of advanced transportation systems
17. Aerodynamic problems of manned space vehicles
18. A cone-wedge waverider configuration for engine-airframe integration
19. Waverider configurations based on nonaxisymmetric flow fields for engine-airframe integration
20. Navier-Stokes computations of hypersonic viscous optimized waveriders
21. Multidisciplinary optimization of airbreathing hypersonic vehicles