Hot gas ingestion test results of a two-poster vectored thrust concept with flow visualization in the NASA Lewis 9- x 15-foot low speed wind tunnel
By: Albert L. Johns, ... [et al.].
Contributors: Johns, Albert L.; Lewis Research Center.
Series: NASA technical memorandum -- 103258.
Publisher: Lewis Research Center
Published: 1990
Place of publication: [Cleveland, Ohio
Language: eng
Format: Microform
Subjects: Control systems design.; Exhaust nozzles.; Flow distribution.; Flow visualization.; High temperature gases.; Inlet flow.; Laser applications.; Nozzle flow.; Support systems.; Thrust vector control.
Notes: "AIAA 90-2268."

Includes bibliographical references.

Also available via Internet from the NTRS web site. Address as of 7/21/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19910011803%5F1991011803.pdf; current access is available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration,] 1991. 1 microfiche.