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Aeroelastic loads prediction for an arrow wing : Task III - evaluation of the boeing three - dimensional leading-edge vortex code

Aeroelastic loads prediction for an arrow wing : Task III - evaluation of the boeing three - dimensional leading-edge vortex code - - Washington, D.C. National Aeronautics and Space Administration 1983 - 218 p. - NASA CR 3642 : 1983 .

ISBN:

Subjects--Topical Terms:

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

Universal Decimal Class. No.: LNASA CR 3642 : 1983

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