| 000 -LEADER |
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| fixed length control field |
02090nam a22003017a 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 |
20220816134547.0 |
| 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 161-170] |
| 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 |
1959 |
| 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 |
|---|
| General note |
NASA TN D-161: An investigation of some aspects of the sonic boom by means of wind tunnel measurements of pressures about several bodies at mach number of 2.01 by Harry W. Carlson 44p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-162: Handbook of structural stability: Part VII strength of thin wing tunnel by George Gerard 83p |
| 500 ## - GENERAL NOTE |
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| General note |
NASA TN D-163: Handbook of structural stability: Supplement to part III buckling of curved plates and shells23p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-164: A radar test target system by James T. Rose 53p |
| 500 ## - GENERAL NOTE |
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| General note |
NASA TN D-165: A brief investigation of the effect of waves on the take off resistance of a seaplane by Elmo J. Mottard 17p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-166: A hydrodynamic investigation of the effect of adding upper surface camber to a submerged flat plate by Victor L. Vaughan 22p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-167: Investigation of variation in base pressure over the reynolds number range in which wake transition occurs for two dimensional bodies at mach numbers from 1.95 to 2.92 by Vernon Van Hise 44p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-168: Static force of several annular jet configurations in proximity to smooth and irregular ground by Edwin E. Davenport 13p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-169: Spectrographic temperature measurements in a carbon arc powered air jet by David H. Greenshields 24p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-170: Lift and drag charectristics at subsonic speeds and at a mach number of 1.9 of a lifting circular cylinder with a fineness ratio of 10 by Vernard E. Lockwood 21p |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Wind tunnel |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
