A new blade element method for calculating the performance of high and intermediate solidity axial flow fans

LDR 01538cam a2200337Ii 4500
001 011431508
003 MiAaHDL
005 20141013010000.0
006 m d
007 cr bn ---auaua
008 791115s1979 dcua b f000 0 eng d
035 ⊔ ⊔ ‡asdr-uiuc6386196
035 ⊔ ⊔ ‡a(OCoLC)5698616
037 ⊔ ⊔ ‡b22161
040 ⊔ ⊔ ‡aGPO ‡cGPO ‡dABC ‡dOCLCQ
049 ⊔ ⊔ ‡aUIUU
050 ⊔ 4 ‡aTL521.3.C6 ‡bA6 no. 3063
074 ⊔ ⊔ ‡a830-H-14 (microfiche)
086 0 ⊔ ‡aNAS 1.26:3063
100 1 ⊔ ‡aBorst, Henry V.
245 1 2 ‡aA new blade element method for calculating the performance of high and intermediate solidity axial flow fans / ‡cHenry V. Borst, Henry V. Borst & Associates.
260 ⊔ ⊔ ‡a[Washington] : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1978.
300 ⊔ ⊔ ‡a48 p. : ‡bill. ; ‡c26 cm.
490 0 ⊔ ‡aNASA contractor report ; ‡vNASA CR-3063
500 ⊔ ⊔ ‡aNov. 1978.
500 ⊔ ⊔ ‡aPrepared for Ames Research Center, under contract NAS2-9079.
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAirplanes ‡xTurbojet engines ‡xBlades.
650 ⊔ 0 ‡aPropellers, Aerial.
710 2 ⊔ ‡aHenry V. Borst & Associates.
710 2 ⊔ ‡aAmes Research Center.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Office.
CID ⊔ ⊔ ‡a011431508
DAT 0 ⊔ ‡a20101027121812.0 ‡b20141013010000.0
DAT 1 ⊔ ‡a20141112173021.0 ‡b2025-01-01T19:26:24Z
DAT 2 ⊔ ‡a2025-01-01T18:30:02Z
CAT ⊔ ⊔ ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ⊔ ⊔ ‡aBK
HOL ⊔ ⊔ ‡0sdr-uiuc6386196 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106680355 ‡sUIU ‡16386196
974 ⊔ ⊔ ‡bUIU ‡cUIUC ‡d20250101 ‡sgoogle ‡uuiug.30112106680355 ‡y1979 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019