| 000 | 00689 a2200157 4500 | ||
|---|---|---|---|
| 100 | _aMiddleton, W. D. | ||
| 245 |
_aAerodynamic design and analysis system for supersonic aircraft [NASA CR-2522 -- CR-2525] _bPart 3 : Computer program description _cW. D. Middleton, L. Lundry and R. G. Coleman |
||
| 260 |
_aWashington, D.C. _bNational Aeronautics and Space Administration [NASA] _c1975 |
||
| 300 | _a94p | ||
| 440 | _aNational Aeronautics and Space Administration [NASA] | ||
| 500 | _aBound with NASA CR-2522 to CR-2525 [Accession Nos : TR014192 to TR014194] | ||
| 650 | _aAnalysis system for supersonic aircraft | ||
| 700 | _aLundry, L. | ||
| 700 | _aColeman, R. G. | ||
| 942 | _cTR | ||
| 999 |
_c564147 _d564147 |
||