A modeling technique for STOVL ejector and volume dynamics
By: C.K. Drummond and W.S. Barankiewicz ; prepared for the 26th Joint Propulsion Conference cosponsored by the AIAA, SAE, ASME, and ASEE, Orlando, Florida, July 16-18, 1990.
Contributors: Barankiewicz, W. S.; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 103167.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 11
Subjects: Short take-off and landing aircraft -- Jet propulsion -- Ejectors -- Mathematical models.; Aircraft configurations.; Computational fluid dynamics.; Mathematical models.; Performance prediction.; Thrust.; V/STOL aircraft.
Notes: Cover title.

Shipping list no.: 90-0893-M.

"AIAA-90-2417."

"E-5539"--P. 1.

Includes bibliographical references (p. 7-8).

Also available via Internet from the NASA Technical Report Server web site. Address as of 1/19/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900013250%5F1990013250.pdf; current access available via PURL.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

505-62-71.