| 000 | 00675pam a2200205a 44500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 245 | 1 | _aNASA Technical Note :EXPERIMENTAL FLUTTER STUDY OF A WING-FUSELAGE CONFIGURATION AT A MACH NUMBER OF 15.4 AND COMPARISON WITH THEORY | |
| 260 |
_bNASA _c1965 _aWashington, D.C. |
||
| 300 | _a46p. | ||
| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note. | ||
| 500 | _a Technical Note D-3041-3050 | ||
| 500 | _aBound Vol. No.83094 contents TR14960-14968 | ||
| 650 | _aHelium Flow -- Investigation | ||
| 700 | _aGoetz, Robert C, | ||
| 700 | _aSewall, John L | ||
| 942 | _cTR | ||
| 999 |
_c400386 _d400386 |
||