Analysis of ejector thrust by integration of calculated surface pressures

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086 0 ‡aY 3.N 21/5:6/1958
100 1 ‡aSanders, John C.
245 1 0 ‡aAnalysis of ejector thrust by integration of calculated surface pressures / ‡cJohn C. Sanders and Virginia L. Brightwell.
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1949.
300 ‡a36 p. : ‡bill. ; ‡c28 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aNational Advisory Committee for Aeronautics ; ‡vno. 1958
500 ‡aNACA TN No. 1958.
500 ‡a"October 1949."
504 ‡aIncludes bibliographical references.
520 3 ‡aThe investigation showed that the thrust augmentation of a primary-jet passage with incompressible fluids is created largely by a pressure force on the surface of a converging secondary passage preceding the mixing zone.
520 3 ‡aAn analysis of the thrust of air ejectors was made for the purpose of revealing the nature of ejector action and the source of its thrust. Cases for both incompressible and compressible fluids were considered.
538 ‡aMode of access: Internet.
650 0 ‡aMathematical analysis. ‡0http://id.loc.gov/authorities/subjects/sh85082116
650 0 ‡aPressure. ‡0http://id.loc.gov/authorities/subjects/sh85106531
650 0 ‡aJet propulsion. ‡0http://id.loc.gov/authorities/subjects/sh85070170
700 1 ‡aBrightwell, Virginia L.
710 1 ‡aUnited States. ‡bNational Advisory Committee for Aeronautics. ‡0http://id.loc.gov/authorities/names/n79060141 ‡1http://id.loc.gov/rwo/agents/n79060141
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
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