Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform /

Bibliographic Details
Corporate Author:	United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Other Authors:	Yip, Long P.
Format:	Government Document Microform Book
Language:	English
Published:	Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; 1990.
Series:	NASA technical memorandum ; 4200.
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.
Online Access:	https://purl.fdlp.gov/GPO/LPS65804

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