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Aeroelastic loads prediction for an arrow wing : Task II - Evaluation of semi-empirical methods

Aeroelastic loads prediction for an arrow wing : Task II - Evaluation of semi-empirical methods - - Washington, D.C. NASA 1983 - 124 p. - NASA CR 3641 : 1983 .

ISBN:

Subjects--Topical Terms:

Aeroelasticity, Experimental pressure distributions, Aerodynamic theory, Arrow-wing configuration, Wind tunnel test

Universal Decimal Class. No.: LNASA CR 3641 : 1983

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