1 |
Schafer, K., Zimmermann, H. and Kruehsel, G., "Altitude Simulation Bench for VINCI Engine," 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Jul. 2003.
|
2 |
Stinnett W.D., "Centerbody Diffuser Study" AEC-NASA Space Nuclear Propulsion Office, Report No. RN-S-0243, Oct. 1965.
|
3 |
Christopher L.C., "High Speed Flight Vehic le Structures : An Overview," Journal of Aircraft, Vol. 41, No. 5, pp. 978-985, 2004.
DOI
ScienceOn
|
4 |
Park, B.H., Lee J.H. and Yoon, W.S., " Studies on the starting transient of a straight cylindrical supersonic exhaust diffuser," international journal of hear and fluid flow, Vol. 29, pp. 1369-1379, Oct. 2008.
DOI
ScienceOn
|
5 |
Sankaran, S., Satyanarayana, T.N.V., Anna malai, K., Visvanathan, K., Babu, V. and Sundararajan, T., "CFD Analysis for Sim ulated Altitude Testing of Rocket Motors," Canadian Aeronautics and Space Journal, Vol. 48, No. 2, 2002.
|
6 |
Fortini, A., "Performance Investigation of a Nonpumping Rocket-Ejector System for Altitude Simulation," NASA TN D-257, 1959.
|
7 |
William L. J., "Experimental Study of Zero -Flow Ejectors Using Gaseous Nitrogen," NASA-TD-203, 1960.
|
8 |
Fluent 14.0, FLUENT Inc.
|
9 |
Fortini, A. and Nucci, L.M., "Preliminary inves tigation of a new type of supersonic inlet," Langley Aeronautical Laboratory, Report-1104, 1965.
|
10 |
Kruehsel, G., Schafer, K., Zimmermann, H. and Pauly, C., "Operation of VINCI Altitude Simulation Test Bench P4.1," Aerospace testing, Munich, Germany, 2008.
|
11 |
Park, B.H., Lim J.H. and Yoon, W.S, "Fuid dynamics in starting and terminating transients of zero-secondary flow ejector," international journal of hear and fluid flow, Vol. 29, pp. 327-339, Feb. 2008.
DOI
ScienceOn
|