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Correlation of the drag characteristics of a typical pursuit airplane obtained from high-speed wind-tunnel and flight tests
In order to obtain a correlation of drag data from wind-tunnel and flight tests at high Mach numbers, a typical pursuit airplane, with the propeller removed, was tested in flight at Mach numbers up to 0.755, and the results were compared with wind-tunnel tests of a 1/3-scale model of the airplane. The tests results show that the drag characteristics of the test airplane can be predicted with satisfactory accuracy from tests in the Ames 16-foot high-speed wind tunnel of the Ames Aeronautical Laboratory at both high and low Mach numbers. It is considered that this result is not unique with the airplane.
Date:
November 2, 1944
Creator:
Nissen, James M.; Gadeberg, Burnett L. & Hamilton, William T.
System:
The UNT Digital Library