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Transonic flow field analysis for wing - fuselage configurations

Transonic flow field analysis for wing - fuselage configurations - - Washington, D.C. NASA 1980 - 158 p. - NASA CR 3243 : 1980 .

ISBN:

Subjects--Topical Terms:

Transonic flow,Computational aerodynamics,Flow simulations,Wing-fuselage,Finite difference relaxation scheme

Universal Decimal Class. No.: LNASA CR 3243 : 1980

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