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Low-Speed Measurements of Static and Oscillatory Lateral Stability Derivatives of a 1/5 Scale Model of a Jet-Powered Vertical-Attitude VTOL Research AirplaneForce tests of the static and dynamic lateral stability characteristics of a VTOL airplane having a triangular wing mounted high on the fuselage with a triangular vertical tail on top of the wing and no horizontal tail have been made in the Langley free-flight tunnel. The static lateral stability parameters and the rolling, yawing, and sideslipping dynamic stability derivatives are presented without analysis.
Document ID
19980235622
Acquisition Source
Headquarters
Document Type
Technical Memorandum (TM)
Authors
Shanks, Robert E. (NASA Langley Research Center Hampton, VA United States)
Smith, Charles C., Jr. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1959
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-TM-X-143
L-640
Report Number: NASA-TM-X-143
Report Number: L-640
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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