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Start Over Partner UNT Libraries Government Documents Department Serial/Series Title Technical note (United States. National Advisory Committee for Aeronautics) Year 1954 Month June

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Tables for the Computation of Wave Drag of Arrow Wings of Arbitrary Airfoil Section (open access)

Tables for the Computation of Wave Drag of Arrow Wings of Arbitrary Airfoil Section

Tables and computing instructions for the rapid evaluation of the wave drag of delta wings and of arrow wings having a ration of the tangent of the trailing-edge sweep angle to the tangent of the leading-edge sweep angle in the range from -1.0 to 0.8. The tables cover a range of both subsonic and supersonic leading edges.
Date: June 1954
Creator: Grant, Frederick C. & Cooper, Morton
System: The UNT Digital Library