1982•Medical Entomology and ZoologyRequires access

Experimental testing at transonic speeds

John Blackwell

Abstract

Nomenclature b = wing span c = wing chord c , = section drag coefficient d c = section lift coefficient c = section normal force coefficient n c = slope of section normal force vs angle-ofa attack curve c = section pitching moment coefficient C = aircraft drag coefficient C = aircraft lift coefficient LI C = pressure coefficient Cju = blowing coefficient M = Mach number P = total pressure q , q = freestream dynamic pressure

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Available abstract

Key concepts: Lift coefficient, Pressure coefficient, Drag coefficient, Chord (peer-to-peer), Pitching moment, Transonic, Freestream, Mach number