Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study. [Part] I, , Design and experimental performance of standard turbine

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100 1 ‡aRohlik, Harold E.
245 1 0 ‡aInvestigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study. ‡n[Part] I, ‡p, Design and experimental performance of standard turbine / ‡cHarold E. Rohlik, William T. Wintucky and Herbert W. Scibbe..
246 1 0 ‡aDesign and experimental performance of standard turbine
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1957.
300 ‡a31 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 ; ‡vE56J16
500 ‡a"January 9, 1957."
504 ‡aIncludes bibliographical references (p. 13-14).
538 ‡aMode of access: Internet.
650 0 ‡aAerodynamics, Supersonic. ‡0http://id.loc.gov/authorities/subjects/sh85001297
650 0 ‡aAxial flow. ‡0http://id.loc.gov/authorities/subjects/sh2002010496
650 0 ‡aTurbines ‡xDesign and construction.
700 1 ‡aScibbe, Herbert W.
700 1 ‡aWintucky, William T.
710 2 ‡aLewis Flight Propulsion Laboratory. ‡0http://id.loc.gov/authorities/names/no2015026965 ‡1http://id.loc.gov/rwo/agents/no2015026965 ‡1http://viaf.org/viaf/314909134
710 2 ‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum.
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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