| 000 -LEADER |
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| fixed length control field |
02059nam 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 |
20220922095318.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
220922b 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 Aeronautis and Space Administration |
| 245 ## - TITLE STATEMENT |
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| Title |
- |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washigton,D.C. |
| Name of publisher |
National Aeronautis and Space Administration |
| Year of publication |
1964 |
| 300 ## - PHYSICAL DESCRIPTION |
|---|
| Number of Pages |
32p |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautis and Space Administration |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
NASA Technical Note |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2381: Effect of wing stalling in transition on a 1/4-scale model of the vz-2 aircraft by Robert O. Schade |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2382: Force test investigation of a 1/4-scale model of the modified vz-2 aircraft by Robert H. Kirby 71p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2383: Heat-transfer rates and ablation on a blunted cylinder-flare configuration in free flight up to a mach number of 8.98 by Clyde W. Winters 27p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2384: Diffuser performance of a mach 6 open-jet tunnel and model-blockage effects at stagnation temperatures to 3,600 F by Raymond E. Midden 23p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2385: Comparison of heat-rejection and weight characteristics of several radiator fin-tube configurations by Henry C. Haller 34p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2386: Heat transfer on unswept and 38 cylindrically blunted wedge fins in free flight to mach number 4.11 by Floyd G. Howard 48p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2387: Heat-transfer and pressure measurements on delta wings at mach numbers of 3.1 and 4.65 and angles of attack from -45 to 45 by Robert L. Stallings 176p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2388: Vectorial reflectance of the explorer IX satellite material by Gerald M. Keating 45p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2389: Supersonic aerodynamic characteristics of a series of bodies having variations in fineness ratio and cross-section ellipticity by Bernard Spencer,Jr. 76p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN-2390: Numerical calculation of supersonic flows of a perfect gas over bodies of revolution at small angles of yaw by John V. Rakich 56p |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
