Citation: | Zou Xinhua, Wang Qiang. Internal performance of counterflow thrust vectoring nozzle under different flight conditions[J]. Journal of Beijing University of Aeronautics and Astronautics, 2011, 37(2): 227-230,236. (in Chinese) |
[1] Strykowski P J, Krothapalli A, Forliti D J.Counterflow thrust vectoring of supersonic jets[R]. AIAA96-0115,1996 [2] Vanderveer M R,Strykowski P J. Counterflow thrust vector control of subsonic jets:continuous and bistable regimes[J]. Journal of Propulsion and Power,1997,13(3):412-413 [3] Hunter C A , Deere K A. Computational investigation of fluidic counterflow thrust vectoring[R]. AIAA99-2669,1999 [4] Barth T J,Jespersen D.The design and application of upwind schemes on unstructured meshes[R]. AIAA89-0366,1989 [5] Choudhury D. Introduction to the renormalization group method and turbulence modeling[R].Fluent Inc Technical Memorandum TM-107,1993 [6] Flamm J D. Experimental study of a nozzle using fluidic counterflow for thrust vectoring[R] . AIAA98-3255,1998
|