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On the determination of certain basic types of supersonic flow fieldsA discussion is given of the application of Fourier series techniques to the problems of linearized supersonic flow. The formulation presented is an extension of the doublet type of "fundamental solution" to higher order types of singularity. The equations developed have application to wing theory but are primarily of importance in wing-body interaction problems. A specific example of a wing-body interference problem is discussed in light of the presented methods.
Document ID
19930093849
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ferrari, Carlo
Date Acquired
August 16, 2013
Publication Date
November 1, 1954
Report/Patent Number
NACA-TM-1381
Report Number: NACA-TM-1381
Accession Number
93R23174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BODIES - AERODYNAMIC THEORY
WING-FUSELAGE COMBINATIONS - AIRPLANES
FLOW, SUPERSONIC
WINGS, COMPLETE - THEORY
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