Analysis of installation performance of the missile turbojet engine

Tuijin Jishu/Journal of Propulsion Technology

Volumn 24, Issue 1, 2003, Pages 12-16

  Wang, Zhan Xue ^a   Qiao, Wei Yang ^a   Cai, Yuan Hu ^a  

^a NORTHWESTERN POLYTECHNICAL UNIVERSITY   (China)

Author keywords

Inlet drag; Installation performance; Nozzle afterbody drag; Numerical calculation; Turbojet engine

Indexed keywords

COMPUTER SIMULATION; DRAG; MISSILES;

INLET DRAG; INSTALLATION PERFORMANCE; MISSILE TURBOJET ENGINE; NOZZLE/AFTERBODY DRAG; NUMERICAL SIMULATION;

TURBOJET ENGINES;

EID: 0037534186     PISSN: 10014055     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (8)

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2. Swavely C E, Soileau J F. Aircraft afterbody/propulsion system integration for low drag [R]. AIAA 72-1101.
3. Kowalski E J. A computer code for estimating installed performance of aircraft fan turbine engines [R]. Vol.1 Final report. NASA CS-159691. 1979.
4. Tong Kaisheng. The thermodynamic calculation of turbofan (Chinese) [R]. Chinese Aviation Press, 1989.
5. Sellers J F, Daniele C J. DYNGEN-a program for calculating steady-state and transient performance of turbojet and turbofan engines [R]. NASA TN D-7901, 1975.