Investigation of intake ducts for a high-speed subsonic jet-propelled airplane

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086 0 ‡aY 3.N21/5:15/L7C24a
100 1 ‡aCohen, Herbert N.
245 1 0 ‡aInvestigation of intake ducts for a high-speed subsonic jet-propelled airplane / ‡cBy Herbert N. Cohen.
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1947.
300 ‡a8 [19] p. : ‡bill. ; ‡c27 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aNational Advisory Committee for Aeronautics research memorandum ; ‡vL7C24a
500 ‡a"April 23, 1947."
504 ‡aIncludes bibliographical references (p. 7).
520 ‡aEffects of roughness, size, and constructional features on efficiency and pressure loss are checked in two intake ducts of different area. Results indicate that larger internal passages increase efficiency. Poor finishing may decrease efficiency by as much as 50%, while spoilers may increase duct pressure los by 700%. Splitter vanes across duct, to insure rigidity, increase pressure loss by about 50%.
538 ‡aMode of access: Internet.
650 0 ‡aJet planes ‡xAir ducts.
650 0 ‡aAir ducts ‡xAerodynamics. ‡0http://id.loc.gov/authorities/subjects/sh85002630
710 2 ‡aLangley Aeronautical Laboratory. ‡0http://id.loc.gov/authorities/names/n81018841 ‡1http://id.loc.gov/rwo/agents/n81018841
710 2 ‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
899 ‡a39015086464271
CID ‡a100167894
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DAT 2 ‡a2024-05-05T17:30:02Z
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