LDR | |
01201cam a2200289Ia 4500 |
001 |
|
011422784 |
003 |
|
MiAaHDL |
005 |
|
20141013010000.0 |
006 |
|
m d |
007 |
|
cr bn ---auaua |
008 |
|
920627s1987 dcua b f000 0 eng d |
035 |
⊔ |
⊔ |
‡asdr-uiuc6342077
|
035 |
⊔ |
⊔ |
‡a(OCoLC)26094151
|
040 |
⊔ |
⊔ |
‡aABC
‡cABC
‡dOCL
|
049 |
⊔ |
⊔ |
‡aUIUU
|
090 |
⊔ |
⊔ |
‡aTL521.3
‡b.N18 no. 2713
|
100 |
1 |
⊔ |
‡aChu, Julio.
|
245 |
1 |
0 |
‡aPressure measurements on a thick cambered and twisted 58 ̊delta wing at high subsonic speeds /
‡cJulio Chu and John E. Lamar.
|
260 |
⊔ |
⊔ |
‡aWashington, D.C. :
‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office ;
‡aSpringfield, Va. :
‡bFor sale by the National Technical Information Service,
‡c1987.
|
300 |
⊔ |
⊔ |
‡a238 p. :
‡bill. ;
‡c28 cm.
|
490 |
⊔ |
0 |
‡aNASA technical paper ;
‡v2713
|
500 |
⊔ |
⊔ |
‡a"September 1987"--Cover.
|
500 |
⊔ |
⊔ |
‡aPrepared at Langley Research Center.
|
504 |
⊔ |
⊔ |
‡aIncludes bibliographical references (p. 9-10).
|
538 |
⊔ |
⊔ |
‡aMode of access: Internet.
|
650 |
⊔ |
0 |
‡aCamber (Aerofoils)
|
650 |
⊔ |
0 |
‡aAirplanes
‡xWings, Triangular
‡xTesting.
|
650 |
⊔ |
0 |
‡aAerodynamic load
‡xMeasurement
‡vStatistics.
|
700 |
1 |
⊔ |
‡aLamar, John E.
|
710 |
2 |
⊔ |
‡aLangley Research Center.
|
CID |
⊔ |
⊔ |
‡a011422784
|
DAT |
0 |
⊔ |
‡a20100927154507.0
‡b20141013010000.0
|
DAT |
1 |
⊔ |
‡a20141112173021.0
‡b2024-01-17T02:05:40Z
|
CAT |
⊔ |
⊔ |
‡aSDR-UIUC
‡dUNKNOWN
‡lloader.pl-003-020
|
FMT |
⊔ |
⊔ |
‡aBK
|
HOL |
⊔ |
⊔ |
‡0sdr-uiuc6342077
‡auiug
‡bSDR
‡cUIUC
‡puiug.30112106605733
‡sUIU
‡16342077
|
974 |
⊔ |
⊔ |
‡bUIU
‡cUIUC
‡d20240117
‡sgoogle
‡uuiug.30112106605733
‡y1987
‡rpd
‡qbib
‡tUS fed doc--NTIS: pubdate < 2018
|