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Tables of Interference Factors for Use in Wind-tunnel and Ground-effect Calculations for VTOL-STOL Aircraft. Part IV- Wind Tunnels Having Width-height Ratio of 0.5Tables 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 0.5. 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
19620000019
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
Computer Operations And Hardware
Report/Patent Number
NASA-TN-D-936
L-1551
Report Number: NASA-TN-D-936
Accession Number
62N10019
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Wind tunnel
STOL aircraft
Interference factor table
VTOL aircraft
Ground effect
IBM 704
IBM 7090

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