NASA technical note [NASA TN D 221-230]
By: Washington: National Aeronautics and Space Administration.
Material type:
BookSeries: National Aeronautics and Space Administration ; NASA Technical Note. Publisher: Washington, D. C. National Aeronautics and Space Administration 1960Subject(s): Subsonic
| Item type | Current location | Collection | Call number | Vol info | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|---|
Technical Report
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PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA Technical note D 221-232 | Not for loan | 63647 |
NASA TN D-221: In flight measurements of the time required for a pilot to respond to an aircraft disturbance by Helmut A. Kuehnel
NASA 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
NASA 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
NASA 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
NASA 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
NASA 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
NASA 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
NASA 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
NASA TN D-229: Expermental investigation of the effect of aspect ratio and mach number on the flutter of catilever wings by E. Widmayer 20p
NASA 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
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