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Low speed wind tunnel test of ground proximity and deck edge effects on a lift cruise fan V/STOL configuration, volume 1The characteristics were determined of a lift cruise fan V/STOL multi-mission configuration in the near proximity to the edge of a small flat surface representation of a ship deck. Tests were conducted at both static and forward speed test conditions. The model (0.12 scale) tested was a four fan configuration with modifications to represent a three fan configuration. Analysis of data showed that the deck edge effects were in general less critical in terms of differences from free air than a full deck (in ground effect) configuration. The one exception to this was when the aft edge of the deck was located under the center of gravity. This condition, representative of an approach from the rear, showed a significant lift loss. Induced moments were generally small compared to the single axis control power requirements, but will likely add to the pilot work load.
Document ID
19790019970
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Stewart, V. R.
(Rockwell International Corp. Columbus, OH, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1979
Subject Category
Aerodynamics
Report/Patent Number
NR79H-12-VOL-1
NASA-CR-152247
Accession Number
79N28141
Funding Number(s)
CONTRACT_GRANT: NAS2-9882
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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