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Tables of Interference Factors for Use in Wind-tunnel and Ground-effect Calculations for VTOL-STOL Aircraft. Part I - Wind Tunnels Having Width-height Ratio of 2.0Tables of interference factors for use in wind-tunnel and ground-effect calculations for VTOL-STOL aircraft are presented for wind tunnels having a width-height ratio of 2.0. These tables were machine-calculated and are intended for use with the procedures of NASA Technical Report R-124. These tables are presented without comment.
Document ID
19620000016
Acquisition Source
Langley Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
Harry H Heyson (Langley Research Center Hampton, Virginia, United States)
Date Acquired
August 1, 2013
Publication Date
January 1, 1962
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TN-D-933
L-1548
Report Number: NASA-TN-D-933
Accession Number
62N10016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Interference factor table
VTOL aircraft
STOL aircraft
Wind tunnel
Ground effect

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