Static investigation of two fluidic thrust-vectoring concepts on a two-dimensional convergent-divergent nozzle
By: David J. Wing.
Contributors: Langley Research Center.
Series: NASA technical memorandum -- 4574.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1994
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Coanda effect.; Computational fluid dynamics.; Convergent-divergent nozzles.; Flow visualization.; Fluidics.; Secondary flow.; Static tests.; Thrust vector control.; Two dimensional models.; Two fluid models.; Wind tunnel tests.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0410-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1995] 3 microfiches.