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Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations

Feasibility of combining linear theory and impact theory methods for the analysis and design of high speed configurations - - Washington, D.C. National Aeronautics & Space Administration 1978 - 39 p. - NASA CR 3069 : 1978 .

ISBN:

Subjects--Topical Terms:

Aerodynamic characteristics, Aerodynamic predictions, Delta wings, Pressure distributions, High speed configurations

Universal Decimal Class. No.: LNASA CR 3069 : 1978

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