Oscillating pressures near a static pusher propeller at tip Mach numbers up to 1.20 with special reference to the effects of the presence of the wing /
Harvey H. Hubbard and Leslie W. Lassiter.

Description

Main Author

Hubbard, Harvey H.

Related Names

Lassiter, Leslie W.
United States. National Advisory Committee for Aeronautics.

Language(s)

English

Published

Washington, D.C. : National Advisory Committee for Aeronautics, 1954.

Subjects

Propellers, Aerial.
Pressure > Pressure / Measurement.
Airplanes > Airplanes / Wings.
Pressure > Pressure / Measurement.
Airplanes > Airplanes / Wings.
Propellers, Aerial.

Summary

Measurements of free-space oscillating presssures near a static propeller in the region where a wing might be located are presented for the tip Mach number range of 0.50 to 1.20 and these results are compared with available theory. Some measurements are also presented which were made near the tipes in the region where a fuselage might be located in order to extend the range of existing data from a tip Mach number of 1.00 to 1.20. In addition to a description of the free-space pressure field, meausrements are given from some of the same field points with a wing in place.

Note

Includes an errata page.
NACA TN No. 3202.
"July 1954."

Physical Description

35, [1] p. : ill. ; 27 cm.

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