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Bumblebee Program: Aerodynamic data. Part 4: Wing loads at Mach numbers 1.5 and 2.0Individual wing panel aerodynamic characteristics are provided for rectangular wings with aspect ratios of 0.25, 0.75, and 1.00 each panel at Mach numbers if 1.5 and 2.0 for angles of attack to 23 degrees. Data plots produced from reports of wind tunnel tests show normal force coefficients, and the spanwise and chordwise center of pressure locations.
Document ID
19790013870
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Barnes, G. A. (Johns Hopkins Univ. Silver Spring, MD, United States)
Cronvich, L. L. (Johns Hopkins Univ. Silver Spring, MD, United States)
Date Acquired
September 3, 2013
Publication Date
April 1, 1979
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3117
Report Number: NASA-CR-3117
Accession Number
79N22041
Funding Number(s)
CONTRACT_GRANT: NASA ORDER L-60036-A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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