Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations
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Calculation of compressible, nonadiabatic boundary layers in laminar, transitional and turbulent flow by the method of integral relations
(NASA contractor report, NASA CR-1797)
National Aeronautics and Space Administration , For sale by the National Technical Information Service, 1971
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Title from cover
Bibliographical references: p. 77-82
"Prepared by Nielsen Engineering and Research, Inc. ... for Langley Research Center."