Theoretical investigation of ducted propeller aerodynamics. Volume IV

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049 ‡aMAIN
086 0 ‡aD 117.8/2:61-120
100 1 ‡aSinacori, J., ‡eauthor.
245 1 0 ‡aTheoretical investigation of ducted propeller aerodynamics. ‡nVolume IV / ‡cby J. Sinacori & A. Lange.
264 1 ‡aFort Eustis, Virginia : ‡bU.S. Army Transportation Research Command, ‡c1961.
300 ‡a108 pages : ‡billustrations ; ‡c25 cm
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aTCREC technical report ; ‡v61-120
500 ‡a"September 1961."
504 ‡aIncludes bibliographical references (page 101)
520 ‡aThe performances of VTOL aircraft using ducted and free propellers are compared The comparison is based on existing light VTOL aircraft equipped with ducted propellers and on the same aircraft using free propellers computed for this purpose. The free propellers appear to provide better aircraft performance, especially higher flight speed. An appraisal and analysis of VTOL aircraft based on the existing VTOL testbeds forms the second part of this volume. Summaries of design particulars and performance re given in graphical and tabular form. The special purpose vehicles, such as the flying jeeps, aerial platforms and aerodynes, are treated as a separate group. Particular performance data of the various VTOL aircraft are collected in an appendix.
536 ‡aPrepared by Republic Aviation Corporation, Farmingdale, New York, under contract no. ‡bDA44-177-TC-674 ‡g9R38-11-009-12
538 ‡aMode of access: Internet.
650 0 ‡aPropellers, Aerial.
650 0 ‡aVertically rising aircraft ‡xAerodynamics.
700 1 ‡aLange, A., ‡eauthor.
710 2 ‡aRepublic Aviation Corporation, ‡esponsor.
710 1 ‡aUnited States. ‡bArmy. ‡bTransportation Research Command, ‡eissuing body.
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