| 000 -LEADER |
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| fixed length control field |
02035nam a22002897a 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 |
20220914121950.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
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| fixed length control field |
220914b 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 |
- |
| 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 TR R-11: An approximation analytical method for studying entry into planetary atmospheres by Dean R. Chapman 44p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R-12: Effect of the proximity of the wing first bending frequency and the short period frequency on the airplane dynamic response factor by Carl R. Huss 20p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R-13: Effect of a stringer concentration due to a crack in a thin sheet by J. Lyell Sanders 10p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R-14: A method for calculation of hydrodynamic lift for submerged and planing rectangular lifting surfaces by Kenneth L. Wadlin 13p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R=15: Approximate analytical solutionsfor hypersonic flow overslender power law bodies by Harold Mirels 24p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R-16: Effects of mach number and wall temperature at mach numbers from 3 to 5 by Thorval Tendeland 15p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R-17: Analysis of turbulent flow and heat transferon a flat plate at high mach numberswith variales fluid properties by R. G. Deissler 33p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R-18: Several methods for aerodynamics reduction of static pressure sensing errors for aircraft at subsonic near sonic andlowsupersoni sppeds by Virgil S.Ritchie 23p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R-19: Theoretical analysisof thr longitudinal behavior of an automaticcaly controlled supersonic intercepeter during the attach phase by Ordway B. Gates 21p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TR R-20: Tire to surface friction coefficient measurements with A C-123B airplaneon various runwaysurfaces by Richard H. Sawyer 32p |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
