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High Reynolds number research - 1980The fundamental aerodynamic questions for which high Reynolds number experimental capability is required were examined. Potential experiments which maximize the research returns from the use of the National Transonic Facility (NTF) were outlined. Calibration plans were reviewed and the following topics were discussed: fluid dynamics; high lit; configuration aerodynamics; aeroelasticity and unsteady aerodynamics; wind tunnel/flight correlation; space vehicles; and theoretical aerodynamics
Document ID
19810022588
Acquisition Source
Legacy CDMS
Document Type
Book
Authors
Mckinney, L. W. (NASA Langley Research Center Hampton, VA, United States)
Baals, D. D. (Joint Inst. for Advancement of Flight Sciences Hampton, Va., United States)
Date Acquired
September 4, 2013
Publication Date
September 1, 1981
Subject Category
Aerodynamics
Report/Patent Number
L-14416
NASA-CP-2183
Accession Number
81N31130
Funding Number(s)
PROJECT: RTOP 505-31-63-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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