| 000 | 01568nam a22002537a 4500 | ||
|---|---|---|---|
| 003 | OSt | ||
| 005 | 20220926100028.0 | ||
| 008 | 220926b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aWashington: National Aeronautics and Space Administration | ||
| 245 | _a- | ||
| 260 |
_aWashington, D. C. _bNational Aeronautics and Space Administration _c1965 |
||
| 500 | _aNASA TN D-3081:A study of the dynamics of airplane breaking systems as affected by tire elasticity and break response by Sidney A. Matterson 54p | ||
| 500 | _aNASA TN D-3082: Anumerical method for calculating near field sonic boom pressure signatutres ny Wilbur D. Middleton 9p | ||
| 500 | _aNASA TN D-3083: Optimized turning vane design for an intake elbow of axial flow compressor by S. Z. Pinckney 27p | ||
| 500 | _aNASA TN D-3084: On the numerical theory of satellites with highly inclined orbits by Peter Musen 26p | ||
| 500 | _aNASA TN D-3085: Achieving ariel II design compatability by Allen L. Franta 55p | ||
| 500 | _aNASA TN D-3086: Solar cycle effects on inner zone protons by R. C. Blanchard 31p ; | ||
| 500 | _aNASA TN D-3088: Aerodymanic characteristics of spherically bluntrd cones at mach numbersfrom 0.5 to 5.0 by Robert V. Owens 51p ; | ||
| 500 | _aNASA TN D-3089: The general instability of ring stiffined corrugated cyclinders under axial compression by John N. Dickson 30p ; | ||
| 500 | _aNASA TN D-3090: Vibration analysis of clustered launch vehicles by Rudolf F. Glaser 51p ; | ||
| 942 | _cTR | ||
| 999 |
_c566169 _d566169 |
||