| 000 | 02411nam a2200301 4500 | ||
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| 003 | OSt | ||
| 005 | 20220810144856.0 | ||
| 008 | 220712b xxu||||| |||| 00| 0 eng d | ||
| 040 | _cIIT Kanpur | ||
| 041 | _aeng | ||
| 110 | _aWashington: National Aeronautics and Space Administration | ||
| 245 | _aNASA technical note [NASA TN D 221-230] | ||
| 260 |
_aWashington, D. C. _bNational Aeronautics and Space Administration _c1960 |
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| 440 | _aNational Aeronautics and Space Administration | ||
| 440 | _aNASA Technical Note | ||
| 500 | _aNASA TN D-221: In flight measurements of the time required for a pilot to respond to an aircraft disturbance by Helmut A. Kuehnel | ||
| 500 | _aNASA TN D-222: An investigation of the role of gaseous diffusion in the oxidation of a metal forming a volatile oxide by Jerry L. Modisette 25p | ||
| 500 | _aNASA TN D-223: Effects of nose corner radii afterbody section deflections and a drogue chute on subsonic motions of manned satellite models of reentry configuration by Willard S. Blanchard 16p | ||
| 500 | _aNASA TN D-224: A technique for firing dynamically scaled missile models in wind tunnels and for measurements rocket motor sound and pressure fluctuations by William J. Alford 43p | ||
| 500 | _aNASA TN D-225: Subsonic wind tunnel investigation of the aerodynamic effects of pivoting a low aspect ratio wing to large yaw angles with respect to the fuselage to increase lift drag ratio by Thomas G. Gainer 20p | ||
| 500 | _aNASA TN D-226: Experimental investigation at a mach number of 3.11 of the lift drag and pitching moment characteristics of five blunt lifting bodies by William Letko 13p | ||
| 500 | _aNASA TN D-227: Effect of eccentry of the lunar orbit oblateness of the earth and solar gravitational fields on lunar trajectories by William H. Michael 37p | ||
| 500 | _aNASA TN D-228: Fixed base simulation study of a pilot"s ability to control a winged satellite vehicle during high drag variable lift entries by John M. Eggleston 60p | ||
| 500 | _aNASA TN D-229: Expermental investigation of the effect of aspect ratio and mach number on the flutter of catilever wings by E. Widmayer 20p | ||
| 500 | _aNASA TN D-232: Experimental determination of the effects of frequency and amplitude of oscillation on the roll stability derivatives for a 60 degree delta wing airplane model by Lewis R. Fisher 47p | ||
| 650 | _aSubsonic | ||
| 942 | _cTR | ||
| 999 |
_c565873 _d565873 |
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