Geometric And Structural Properties Of A Rectangular Supercritical Wing Oscillated In Pitch For Measurement Of Unsteady Transonic Pressure Distributions


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Computational Test Cases for a Rectangular Supercritical Wing Undergoing Pitching Oscillations


Computational Test Cases for a Rectangular Supercritical Wing Undergoing Pitching Oscillations

Author: Robert M. Bennett

language: en

Publisher:

Release Date: 1999


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NASA Technical Memorandum


NASA Technical Memorandum

Author:

language: en

Publisher:

Release Date: 1992


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