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Two-Dimensional, Supersonic, Linearized Flow with Heat AdditionCalculations are presented for the forces on a thin supersonic wing underneath which the air is heated. The analysis is limited principally to linearized theory but nonlinear effects are considered. It is shown that significant advantages to external heating would exist if the heat were added well below and ahead of the wing.
Document ID
19980227969
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Lomax, Harvard (NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1959
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-MEMO-1-10-59A
Report Number: NASA-MEMO-1-10-59A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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