Experimental study of a nozzle using fluidic counterflow for thrust vectoring

Experimental study of a nozzle using fluidic counterflow for thrust vectoring

Author(s):: Flamm, Jeffrey D. ( NASA Langley Research Center )
Publication title:: AIAA paper
Title of ser.:: AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:: 1998
Pub. Year:: 1998
No.:: 98-3255
Paper no.:: 98-3255
Page(from):: 1
Page(to):: 27
Pub. info.:: American Institute of Aeronautics and Astronautics
ISSN:: 01463705
Language:: English
Call no.:: A07400
Type:: Technical Paper

Details

TDL ID:	ZA00050858
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	34th
Conf. info. (Venue):	Cleveland, OH
Conf. info. (Date):	1998.07.13-1998.07.15
Note for article:	34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 13-15, 1998/Cleveland, OH

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