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An experimental investigation of dynamic ground effectExperimental studies were conducted to determine the longitudinal force and moment aerodynamic coefficients for a 1/48 scale model of an F-106 aircraft and a 0.01 scale model of an XB-70-1 aircraft. The two airplanes and one 60 degree delta wing model were designed and fabricated to satisfy the specific test conditions of the Kansas University wind tunnel with a 3 by 4.3 test section. Results of the tests are given
Document ID
19870017425
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lee, Pai Hung (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Lan, C. Edward (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Muirhead, Vincent U. (Kansas Univ. Center for Research, Inc. Lawrence, KS, United States)
Date Acquired
September 5, 2013
Publication Date
April 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
CRINC-FRL-717-1
NASA-CR-180305
NAS 1.26:180305
Report Number: CRINC-FRL-717-1
Report Number: NASA-CR-180305
Report Number: NAS 1.26:180305
Accession Number
87N26858
Funding Number(s)
CONTRACT_GRANT: NAG1-616
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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