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 · Leslie W. Lassiter
Jan 1954 · National Advisory Committee for Aeronautics
Ebook
35
Pages
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About this ebook
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.
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