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Aerodynamic characteristics of a V/STOL TRANSPORT model with lift and lift-cruise fan power plantsThe aerodynamic characteristics of lift fans mounted ahead of the wing, rotating cruise fans, and tandem mounted lift fans faired into the wing have been studied. The tests results indicated that the complete configurations, that is, the lift-cruise fan and tandem lift fan configurations, had generally acceptable aerodynamic characteristics. The positive induced lift due to fan flow interference with the airplane flow field was a small percentage of the installed thrust but was adequate to provide significant increases in payload with STOL operation.
Document ID
19660015324
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
David H. Hickey
(Ames Research Center Mountain View, California, United States)
Jerry V. Kirk
(Ames Research Center Mountain View, California, United States)
Leo P. Hall
(Ames Research Center Mountain View, California, United States)
Date Acquired
August 3, 2013
Publication Date
April 4, 1966
Publication Information
Publication: Conference on V/STOL and STOL aircraft
Publisher: National Aeronautics and Space Administration
Volume: NASA-SP-116
Issue Publication Date: January 1, 1966
URL: https://ntrs.nasa.gov/citations/19660015317
Subject Category
Aircraft
Meeting Information
Meeting: Conference on V/STOL and STOL aircraft
Location: Mountain View, CA
Country: US
Start Date: April 4, 1966
End Date: April 5, 1966
Sponsors: Ames Research Center
Accession Number
66N24613
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
JET TRANSPORT
TRANSPORT AIRCRAFT
AERODYNAMIC CHARACTERISTICS
LIFT FAN
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