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Similitude requirements and scaling relationships as applied to model testingThe similitude requirements for the most general test conditions are presented. These similitude requirements are considered in relation to the scaling relationships, test technique, test conditions (including supersonic flow), and test objectives. Particular emphasis is placed on satisfying the various similitude requirements for incompressible and compressible flow conditions. For free flying models tests, the test velocities for incompressible flow are scaled from Froude number similitude requirements and those for compressible flow are scaled from Mach number similitude requirements. The limitations of various test techniques are indicated, with emphasis on the free flying model.
Document ID
19790022005
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Wolowicz, C. H.
(NASA Langley Research Center Hampton, VA, United States)
Brown, J. S., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Gilbert, W. P.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1979
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
H-1022
NASA-TP-1435
Accession Number
79N30176
Funding Number(s)
PROJECT: RTOP 505-06-34
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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