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Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° / by H. Clyde McLemore and Michael D. Cannon.

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Record details

  • Physical Description: 1 online resource (62 pages) : illustrations.
  • Publisher: Washington, [D.C.] : National Advisory Committee for Aeronautics, 1954.

Content descriptions

General Note:
"June 1954."
No Federal Depository Library Program (FDLP) item number.
Bibliography, etc. Note:
Includes bibliographical references (page 15).
Source of Description Note:
Description based on online resource, PDF version; title from title page (TRAIL, viewed August 5, 2020).
Subject: Angle of attack (Aerodynamics)
Mathematical analysis.
Propellers, Aerial > Testing.
Wind tunnel testing.
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LDR 02204nam a2200409Ii 4500
001on1104148279
003OCoLC
00520200824084829.0
006m o d f
007cr bn|||||||||
008190610s1954 dcua gob f000 0 eng d
040 . ‡aTRAAL ‡beng ‡erda ‡epn ‡cTRAAL ‡dOCLCO ‡dTRAAL ‡dOCLCF ‡dGPO ‡dMvI
074 . ‡a9999 (online)
0860 . ‡aY 3.N 21/5:6/3228
1001 . ‡aMcLemore, H. Clyde, ‡eauthor. ‡0(EG-IN)1275084
24510. ‡aAerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0° to 180° / ‡cby H. Clyde McLemore and Michael D. Cannon.
2463 . ‡aAerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 degrees to 180 degrees
264 1. ‡aWashington, [D.C.] : ‡bNational Advisory Committee for Aeronautics, ‡c1954.
300 . ‡a1 online resource (62 pages) : ‡billustrations.
336 . ‡atext ‡btxt ‡2rdacontent
337 . ‡acomputer ‡bc ‡2rdamedia
338 . ‡aonline resource ‡bcr ‡2rdacarrier
4901 . ‡aTechnical notes / National Advisory Committee for Aeronautics ; ‡vNo. 3228
588 . ‡aDescription based on online resource, PDF version; title from title page (TRAIL, viewed August 5, 2020).
500 . ‡a"June 1954."
500 . ‡aNo Federal Depository Library Program (FDLP) item number.
504 . ‡aIncludes bibliographical references (page 15).
650 0. ‡aAngle of attack (Aerodynamics) ‡0(EG-IN)962200
650 0. ‡aMathematical analysis. ‡0(EG-IN)573180
650 0. ‡aPropellers, Aerial ‡xTesting.
650 0. ‡aWind tunnel testing. ‡0(EG-IN)1018265
7001 . ‡aCannon, Michael D., ‡d1968- ‡eauthor.
7101 . ‡aUnited States. ‡bNational Advisory Committee for Aeronautics, ‡eissuing body. ‡0(EG-IN)1039303
77608. ‡iPrint version: ‡aMcLemore, H. Clyde, ‡tAerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees ‡w(OCoLC)671655403
830 0. ‡aTechnical note (United States. National Advisory Committee for Aeronautics) ; ‡v3228. ‡0(EG-IN)1504386
85640. ‡uhttps://purl.fdlp.gov/GPO/gpo142569 ‡9STLIB-IND
949 . ‡hONLINE
901 . ‡aon1104148279 ‡bOCoLC ‡c22024008 ‡tbiblio ‡sGPO - Government Documents

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