Accession Number : ADA298731

Title :   The Reversibility Theorem for Thin Airfoils in Subsonic and Supersonic Flow.

Corporate Author : NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON DC

Personal Author(s) : Brown, Clinton E.

PDF Url : ADA298731

Report Date : 1950

Pagination or Media Count : 8

Abstract : NO ABSTRACT DUE TO ILLEGIBILITY OF REPORT

Descriptors :   *AIRFOILS, *REVERSIBLE, *SUBSONIC FLOW, *SUPERSONIC FLOW, THINNESS, THEOREMS.

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE