Moveable cowl control for increased hypersonic performance

8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1998, Pages 1-11

  Rudd, Lael Voneggers ^a   Rankins, Falcon ^a   Pines, Darryll J ^a  

^a UNIVERSITY OF MARYLAND   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ORBITAL TRANSFER; SPACECRAFT;

DESIGN PERFORMANCE; ENGINE INLETS; GLOBAL EFFECTS; NOVEL CONCEPT; OFF DESIGNS; OFF-DESIGN PERFORMANCE; PITCH CONTROL; VEHICLE DESIGN;

DESIGN;

EID: 84983200542     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. Takashima, N., Lewis, M. J., and Lockwood, M. K., "Waverider Configuration Development for the Dual Fuel Vehicle," AIAA 7th International Space Planes and Hypersonic Systems and Technologies Conference, November 1996.
2. vonEggers Rudd, L. and Lewis, M. J., "Comparison of Shock Calculation Methods," to appear in Journal of Aircraft, July-August 1998
3. Frame, M. J., "Analytical Solutions of Hypersonic Type IV Shock Interactions," PhD Thesis, University of Maryland, College Park, 1998
4. Moeckel, W. E., "Approximate Method for Predicting Form and Location of Detached Shock Waves Ahead of Plane or Axially Symmetric Bodies," NACA TN D-1921, July 1949.
5. Shapiro, A. H., "The Dynamics and Thermodynamics of Compressible Fluid Flow," New York: John Wiley & Sons, 1953.
6. Anderson, J. D., "Modern Compressible Flow with Historical Perspective," New York: McGraw Hill, Inc., 1990.
7. Tarpley, C., "The Optimization of Engine-Integrated Hypersonic Waveriders with Steady State Flight and Static Margin Constraints," PhD Thesis, University of Maryland, College Park, 1995