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| LEADER |
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| 001 |
in00000093911 |
| 005 |
20150927070231.0 |
| 008 |
800404s1963 enka b f00010 eng d |
| 035 |
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|a (OCoLC)06169746
|
| 035 |
|
|
|9 AAL5764AM
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| 040 |
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|a TXA
|c TXA
|d UtOrBLW
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| 049 |
|
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|a TXAM
|c [1147082]
|
| 090 |
|
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|a TL526.G7
|b A4 no. 3289
|
| 100 |
1 |
|
|a Smith, Jeremy H. B.
|
| 245 |
1 |
4 |
|a The use of conical camber to produce flow attachment at the leading edge of a delta wing and to minimize life-dependent drag at sonic and supersonic speeds /
|c by J. H. B. Smith and K. W. Mangler.
|
| 264 |
|
1 |
|a London :
|b Her Majesty's Stationery Office,
|c 1963.
|
| 300 |
|
|
|a 32 pages :
|b illustrations
|
| 336 |
|
|
|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a unmediated
|b n
|2 rdamedia
|
| 338 |
|
|
|a volume
|b nc
|2 rdacarrier
|
| 490 |
1 |
|
|a [Great Britain] Aeronautical Research Council. Reports and memoranda,
|v no. 3289
|
| 500 |
|
|
|a Cover title.
|
| 504 |
|
|
|a Bibliography: page 15.
|
| 650 |
|
0 |
|a Camber (Aerofoils)
|
| 650 |
|
0 |
|a Airplanes
|x Wings, Triangular.
|
| 700 |
1 |
|
|a Mangler, K. W.
|
| 830 |
|
0 |
|a Reports and memoranda (Aeronautical Research Council (Great Britain)) ;
|v no. 3289.
|
| 999 |
|
|
|a MARS
|
| 999 |
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|i 00c91da4-8dd1-3857-ac13-57999571b7d1
|t 0
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| 952 |
f |
f |
|p ric
|a Texas A&M University
|b Rellis Campus
|c Joint Library Facility
|d Remote Storage
|t 0
|e TL526.G7 A4 no. 3289
|h Library of Congress classification
|i unmediated -- volume
|m A14805535633
|
| 998 |
f |
f |
|a TL526.G7 A4 no. 3289
|t 0
|l Remote Storage
|