| 000 -LEADER |
|---|
| fixed length control field |
02136nam a22003017a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
|---|
| control field |
OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20220722145002.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
220722b xxu||||| |||| 00| 0 eng d |
| 040 ## - CATALOGING SOURCE |
|---|
| Transcribing agency |
IIT Kanpur |
| 041 ## - LANGUAGE CODE |
|---|
| Language code of text/sound track or separate title |
eng |
| 110 ## - MAIN ENTRY--CORPORATE NAME |
|---|
| Corporate name or jurisdiction name as entry element |
Washington: National Aeronautics and Space Administration |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
NASA technical note [NASA TN 2971-2980] |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington, D. C. |
| Name of publisher |
National Aeronautics and Space Administration |
| Year of publication |
1953 |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautics and Space Administration |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
NASA Technical Report |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2971: Impingement of water droplets on wedges and diamond airfoils at supersonic speeds by John S. Serafini 62p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2972: Theoretical pressure distributions and wave drags for conical bottalls by John R. Jack 14p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2973: Effect of prestraining on recrystallization temperature and mechanical properties of commercial sintered brought molybdenum by Kenneth C. Dike 25p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2974: Experiments on mixed free and forced convective heat transfer connected with turbulent flow through a short tube by E. R. G. Eckert 59p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2975: Structural efficiences of various aluminium titanium and steel alloys at elevated temperatures by George J. Heimerl 16p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2976: A study of the stability of the incompressible laminar boundary layer on infinite wedges by Neal Tetervin 41p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2977: Techniques for calculating parameters of nonlinear dynamic systems from response data by Benjamin R. Briggs 65p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2978: An approximate method of calculating the deformations of wing having swept M or W, A, and swept-tip plan forms by George W. Zender 28p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2979: Effects of symmetric and asymmetric thrust reversal on the aerodynamic characteristics of a model of a twin engine airplane by Kenneth W. Goodson 67p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN 2980: The aerodynamic characteristics of an aspect ratio 20 wing having thick airfoil sections and employing boundary layer control by suction by Bennie W. Cocke 63p |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Boundary layer |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
