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Tables of Interference Factors for Use in Wind-tunnel and Ground-effect Calculations for VTOL-STOL Aircraft. Part II - Wind Tunnels Having Width-height Ratio of 1.5
Interference factor tables for wind-tunnel and ground-effect calculations for vtol-stol aircraft part ii - width-height ratio 1.5
Document ID
19620000017
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-934
L-1549
Report Number: NASA-TN-D-934
Accession Number
62N10017
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Interference factor table
Wind tunnel
VTOL aircraft
Ground effect
STOL aircraft

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