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Sting-support interference on longitudinal aerodynamic characteristics of cargo-type airplane models at Mach 0.70 to 0.84Transonic pressure tunnel tests to determine effects of sting-support interference on longitudinal aerodynamic characteristics of transport aircraft models with upswept aft ends
Document ID
19670021725
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Loving, D. L. (NASA Langley Research Center Hampton, VA, United States)
Luoma, A. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1967
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4021
Accession Number
67N31054
Funding Number(s)
CONTRACT_GRANT: 126-13-01-39-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FUSELAGE
AIRCRAFT MODEL
AERODYNAMIC CHARACTERISTICS
PRESSURE TUBE
TRANSPORT AIRCRAFT

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