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|a B69-22124
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|a 0114702322
|c 22/6
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|c [1024249]
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|a TL526.G7
|b A4 no. 3573
|
| 082 |
0 |
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|a 629.13/008 s
|a 629.132/362
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| 100 |
1 |
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|a Taylor, A. S.
|
| 245 |
1 |
4 |
|a The formulation of an influence-coefficient method for determining static aeroelastic effects :
|b and its application to a slender aircraft in symmetric flight at M = 2.2 /
|c by A. S. Taylor and D. J. Eckford.
|
| 246 |
3 |
1 |
|a 2.2
|
| 264 |
|
1 |
|a London :
|b H.M.S.O.,
|c 1969.
|
| 300 |
|
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|a 1 unnumbered page, 36 pages, 37-50 pages of 36 illustrations ;
|c 28 cm.
|
| 336 |
|
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|a text
|b txt
|2 rdacontent
|
| 337 |
|
|
|a unmediated
|b n
|2 rdamedia
|
| 338 |
|
|
|a volume
|b nc
|2 rdacarrier
|
| 490 |
1 |
|
|a Aeronautical Research Council. Reports and memoranda, no. 3573
|
| 500 |
|
|
|a Cover title.
|
| 504 |
|
|
|a Bibliography: page 26.
|
| 650 |
|
0 |
|a Aeroelasticity.
|
| 650 |
|
0 |
|a Aerodynamics, Supersonic.
|
| 650 |
|
0 |
|a Supersonic transport planes.
|
| 700 |
1 |
|
|a Eckford, Duncan John.
|
| 830 |
|
0 |
|a Reports and memoranda (Aeronautical Research Council (Great Britain)) ;
|v no. 3573.
|
| 999 |
|
|
|a MARS
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| 999 |
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|a Texas A&M University
|b Rellis Campus
|c Joint Library Facility
|d Remote Storage
|t 0
|e TL526.G7 A4 no. 3573
|h Library of Congress classification
|i unmediated -- volume
|m A14805538089
|
| 998 |
f |
f |
|a TL526.G7 A4 no. 3573
|t 0
|l Remote Storage
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