Journal of the aeronautical sciences. [REQUEST TITLE] · 1950 · 113 citations · 1 references
EngineeringAerospace EngineeringPhysicsAerodynamicsFluid DynamicsFluid MechanicsAirfoil TheoryComputational AerodynamicsTransonic AerodynamicsDragFlow Around AirfoilsFlow Over AirfoilsMach NumberMach Number EffectsTransonic FlowTransonic Similarity Rule
Abstract : The flow over a wedge-shaped profile at zero angle of attack and with a free stream Mach number of one is computed using the hodograph method as simplified by the transonic law of similarity. Drag coefficients are computed for several profiles. (Author)
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