Calibration of a newly developed direct-connect high-enthalpy supersonic combustion research facility

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

Volumn , Issue , 1998, Pages 1-8

  Jackson, K ^a   Gruber, M ^a   Mathur, T ^b   Streby, G ^b   Smith, C ^c   Billig, F ^d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b Taitech Inc   (United States)

^c INNOVATIVE SCIENTIFIC SOLUTIONS INC   (United States)

^d PYRODYNE Inc   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CALIBRATION; COMBUSTORS; ENTHALPY; FLIGHT DYNAMICS; FLIGHT SIMULATORS; FUEL INJECTION; HEAT SINKS; NOZZLES; PROBES; SUPERSONIC AIRCRAFT;

DYNAMIC PRESSURES; PARAMETRIC SPACES; PERFORMANCE PARAMETERS; SIMULATED FLIGHT; STATIC PRESSURE MEASUREMENTS; SUPERSONIC COMBUSTION; VARIABLE GEOMETRY; WRIGHT-PATTERSON AIR FORCE BASE;

COMBUSTION;

EID: 84983185756     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-1510     Document Type: Conference Paper

References (3)

1. Pandolfini, P. P., Billig, F. S., Corpening, G. P., Corda, S., and Friedman, M. A., "Analyzing Hypersonic Engines Using the Ramjet Performance Analysis Code," APL Technical Review, Vol. 2, No. 1, 1990, pp. 68-79.
2. Pandolfini, P. P., and Friedman, M. A., "Instructions for Using Ramjet Performance Analysis (RJPA) - IBM-PC Version 1.24," JHU/APL, AL-92-P175, 1992.
3. Thompson, M. W., "Equilibrium Chemistry Steam Calorimetry Data Analysis Procedure Using the Ramjet Performance Analysis Code," JHU/APL, RTDC-TPS-028, 1997.