Estimated lift and drag characteristics of four wings at supersonic speeds
Entry/Object ID
3449
Category
Report - Technical
Archive Items Details
Description
Empirical methods of estimating the lift and drag characteristics of untwisted and uncambered wings at supersonic speeds have been developed in the Aerodynamics Laboratory. These methods are applied in the present note to the estimation of the characteristics of four wings at present undergoing force tests in the 10-inch supersonic tunnel.
