Low-speed wind-tunnel study of reaction control-jet effectiveness for hover and transition of a STOVL fighter concept /

Bibliographic Details
Main Author:	Riley, Donald R.
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Shah, Gautam H., Kuhn, Richard E.
Format:	Government Document Microform Book
Language:	English
Published:	[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1989.
Series:	NASA technical memorandum ; 4147.
Subjects:	Short take-off and landing aircraft. Vertically rising aircraft. Airplanes > Control systems > Testing. Attitude control. Fighter aircraft. Hovering. Jet flow. Short takeoff aircraft. Wind tunnel tests.
Online Access:	https://purl.fdlp.gov/GPO/LPS72303

Description
Item Description:	"December 1989." "Performing organization report number: L-16616"--Technical rept. documentation p. Shipping list number: 90-0669-M. Microform.
Physical Description:	36 pages : illustrations ; 28 cm. Also available via Internet from the NASA Technical Report Server web site. Address as of 7/28/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900002435%5F1990002435.pdf; current access available via PURL.
Bibliography:	Includes bibliographical references (page 11).