Method for calculating induced velocities at the blades of a slightly inclined propeller with constant circulation

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086 0 ‡aNAS 1.14:D-818
088 ‡aNAS-TN-D-818
100 1 ‡aHeyson, Harry H.
245 0 0 ‡aMethod for calculating induced velocities at the blades of a slightly inclined propeller with constant circulation. / ‡cby Harry H. Heyson
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce], ‡c[1961]
300 ‡a59 p. : ‡bill. ; ‡c26 cm.
490 0 ‡aNASA technical note ; ‡vNASA TN D-818
500 ‡aCover title.
500 ‡a"May 1961."
500 ‡aPropulsion systems, air-jet.
504 ‡aIncludes bibliographical references.
538 ‡aMode of access: Internet.
650 7 ‡aPropulsion systems, air-jet ‡2nasat
710 2 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011445232
DAT 0 ‡a20101105144752.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2025-01-01T19:19:31Z
DAT 2 ‡a2025-01-01T18:30:02Z
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