Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform
By: Long P. Yip ... [et al.].
Contributors: Yip, Long P.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Division.
Series: NASA technical memorandum -- 4200
Publisher: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division; 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: 32
Subjects: Drone aircraft -- Testing.; Airplanes -- Wings, Triangular.; Airplanes -- Handling characteristics.; Aerodynamic configurations.; Controllability.; Flight characteristics.; Flight tests.; Low speed wind tunnels.; Remotely piloted vehicles.; Wind tunnel tests.
Notes: Includes bibliographical references (p. 7).

Also available via Internet from the NASA Technical Report Server web site. Address as of 12/21/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900014927%5F1990014927.pdf ; current access is available via PURL.

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