The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms PDF Download

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The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms

The Calculation of Downwash Behind Supersonic Wings with an Application to Triangular Plan Forms PDF Author: Max A. Heaslet
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 726

Book Description
A method is developed, consistent with the assumptions of small perturbation theory, which provides a means of determining for a known load distribution, the downwash behind a wing in supersonic flow. THe analysis is based upon the use of supersonic doublets which are distributed over the plan form and wake of the wing in a manner determined from the wing loading.
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