| Tag |
First Indicator |
Second Indicator |
Subfields |
| LEADER |
00000cam a2200000 4500 |
| 001 |
in00000096877 |
| 005 |
20150925090529.0 |
| 008 |
800401s1961 enka b f00010 eng d |
| 035 |
|
|
|a (OCoLC)06157109
|
| 035 |
|
|
|9 AAL2590AM
|
| 040 |
|
|
|a TXA
|c TXA
|d UtOrBLW
|
| 049 |
|
|
|a TXAM
|c [1016179]
|
| 090 |
|
|
|a TL526.G7
|b A4 no. 3196
|
| 100 |
1 |
|
|a Roper, G. M.
|
| 245 |
1 |
0 |
|a Use of camber and twist to produce low-drag delta or swept-back wings, without leading-edge singularities, at supersonic speeds /
|c by G. M. Roper.
|
| 264 |
|
1 |
|a London :
|b Her Majesty's Stationery Office,
|c 1961.
|
| 300 |
|
|
|a 54 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. 3196
|
| 500 |
|
|
|a Cover title.
|
| 504 |
|
|
|a Bibliography: page 20.
|
| 650 |
|
0 |
|a Airplanes
|x Wings, Swept-back.
|
| 650 |
|
0 |
|a Aerodynamics, Supersonic.
|
| 830 |
|
0 |
|a Reports and memoranda (Aeronautical Research Council (Great Britain)) ;
|v no. 3196.
|
| 999 |
|
|
|a MARS
|
| 999 |
f |
f |
|s 04bef183-34cd-3e20-9067-a3a62ba219d0
|i 64dc4446-0191-36cc-8da7-b6bbcf0ba6ac
|t 0
|
| 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. 3196
|h Library of Congress classification
|i unmediated -- volume
|m A14805534962
|
| 998 |
f |
f |
|a TL526.G7 A4 no. 3196
|t 0
|l Remote Storage
|