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Wing-body interference at supersonic speeds with an application to combinations with rectangular wings
Report presenting the development of an exact theoretical method that permits the determination of the pressure field of a wing-body combination with a circular body and a wing with supersonic leading and trailing edges. Detailed calculations were performed for wing-body combinations composed of rectangular wings mounted at incidence on bodies at zero angle of attack for effective chord-radius ratios of 4 or less.
Date:
April 1952
Creator:
Nielsen, Jack N. & Pitts, William C.
Object Type:
Report
System:
The UNT Digital Library