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

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049 ‡aMAIN
086 0 ‡aY 3.N 21/5:6/3202
100 1 ‡aHubbard, Harvey H.
245 1 0 ‡aOscillating 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 / ‡cHarvey H. Hubbard and Leslie W. Lassiter.
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1954.
300 ‡a35, [1] p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNational Advisory Committee for Aeronautics technical note ; ‡v3202
500 ‡aIncludes an errata page.
500 ‡aNACA TN No. 3202.
500 ‡a"July 1954."
504 ‡aIncludes bibliographical references.
520 3 ‡aMeasurements 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.
538 ‡aMode of access: Internet.
650 7 ‡aPropellers, Aerial. ‡2fast ‡0(OCoLC)fst01079099
650 7 ‡aPressure ‡xMeasurement. ‡2fast ‡0(OCoLC)fst01075934
650 7 ‡aAirplanes ‡xWings. ‡2fast ‡0(OCoLC)fst00803545
650 0 ‡aPressure ‡xMeasurement.
650 0 ‡aAirplanes ‡xWings.
650 0 ‡aPropellers, Aerial.
700 1 ‡aLassiter, Leslie W.
710 1 ‡aUnited States. ‡bNational Advisory Committee for Aeronautics.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015095016716
CID ‡a100903195
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