An experimental and computational investigation of a translating throat single expansion-ramp nozzle

32nd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1996, Pages

  Deere, Karen A ^a   Asbury, Scott C ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; EXPANSION; NASA; NAVIER STOKES EQUATIONS; NOZZLE DESIGN; NOZZLES; PROPULSION; TEST FACILITIES; TURBULENCE MODELS;

COMPUTATIONAL INVESTIGATION; COMPUTATIONAL STUDIES; FLOW CHARAC-TERISTICS; FREESTREAM CONDITIONS; NASA LANGLEY RESEARCH CENTER; NOZZLE PRESSURE RATIO; OFF-DESIGN PERFORMANCE; TWO-DIMENSIONAL SIMULATIONS;

MACH NUMBER;

EID: 84961933393     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

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3. Carboni, Jeanne D.; Shyne, Rickey J.; Leavitt, Laurence D.; Taylor, John G.; and Lamb, Milton: Supersonic Investigation of Two-Dimensional Hypersonic Exhaust Nozzles. NASA TM-105687, October 1992.
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5. Bare, E. Ann; and Capone, Francis J.: Static Internal Performance of Convergent Single- Expansion-Ramp Nozzles With Various Combinations of Internal Geometric Parameters. NASA TM-4112, May 1989.
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10. Mercer, Charles E.; Berrier, Bobby L.; Capone, Francis J.; and Grayston, Alan M.: Data Reduction Formulas for the 16-Foot Transonic Tunnel NASA Langley Research Center, Revision 2. NASA TM 107646, 1992.
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12. Abdol-Hamid, Khaled S.: Implementation of Algebraic Stress Models in a General 3-D Navier- Stokes Code Method (PAB3D). NASA CR-4702, December 1995.
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15. Ames Res. Staff: Equations, Tables, and Charts for Compressible Flow. NACA Rep. 1135, 1953