| 000 -LEADER |
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| fixed length control field |
02411nam a2200301 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
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| control field |
OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
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| control field |
20220810144856.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
220712b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE |
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| Transcribing agency |
IIT Kanpur |
| 041 ## - LANGUAGE CODE |
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| Language code of text/sound track or separate title |
eng |
| 110 ## - MAIN ENTRY--CORPORATE NAME |
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| Corporate name or jurisdiction name as entry element |
Washington: National Aeronautics and Space Administration |
| 245 ## - TITLE STATEMENT |
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| Title |
NASA technical note [NASA TN D 221-230] |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
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| Place of publication |
Washington, D. C. |
| Name of publisher |
National Aeronautics and Space Administration |
| Year of publication |
1960 |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautics and Space Administration |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
NASA Technical Note |
| 500 ## - GENERAL NOTE |
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| General note |
NASA TN D-221: In flight measurements of the time required for a pilot to respond to an aircraft disturbance by Helmut A. Kuehnel |
| 500 ## - GENERAL NOTE |
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| General note |
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 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 500 ## - GENERAL NOTE |
|---|
| General note |
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 |
| 500 ## - GENERAL NOTE |
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| General note |
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 |
| 500 ## - GENERAL NOTE |
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| General note |
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 |
| 500 ## - GENERAL NOTE |
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| General note |
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 |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Subsonic |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
