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Dynamic Tests of V/STOL Transport ModelsThis paper presents a summary of results obtained in dynamic tests of free-flight models of various configurations suitable for V/STOL transport aircraft at the NASA Langley Research Center. The configurations covered will be the tilt-wing propeller-driven type as represented by the XC-142A tri-service transport, the fan-in-wing type as represented by the XV-5A research airplane, and the jet-lift type as represented by the Dornier 00-31 transport. The test techniques themselves are not described in this paper since they have been described in detail previously in references 1 and 2.
Document ID
19640017732
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Marion O McKinney (Langley Research Center Hampton, Virginia, United States)
Robert H Kirby (Langley Research Center Hampton, Virginia, United States)
Date Acquired
September 2, 2013
Publication Date
August 10, 1964
Publication Information
Publisher: American Institute of Aeronautics and Astronautics
DOI: 10.2514/6.1964-619
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
AIAA-64-619
Meeting Information
Meeting: AIAA Transport Aircraft Design and Operations Meeting
Location: Seattle, WA
Country: US
Start Date: August 10, 1964
End Date: August 12, 1964
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
64N27646
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Dynamic stability
V/STOL aircraft
Transport aircraft

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