| 000 -LEADER |
|---|
| fixed length control field |
02048nam a2200289 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
|---|
| control field |
OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20220907120702.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
220907b 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 Administrtion |
| 245 ## - TITLE STATEMENT |
|---|
| Title |
- |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| Place of publication |
Washington, D. C. |
| Name of publisher |
National Aeronautics and Space Administrtion |
| Year of publication |
1972 |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
National Aeronautics and Space Administrtion |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE |
|---|
| Title |
NASA Technical Note |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6900: Effect of stabilization on vtol aircraft in hovering flight by Richard K. Greif 19p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6901: Atmospheric electricity criteria guidelines for use in aerospace vehicle development by Glenn E. Daniels 18p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6902: The interaction of moderately strong shock waves with thick perforated walls of low porosity by Daniel J. Grant 69p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6903: An ethological study of phthalate self contamination of spacecraft and contamination from their earthly environs by Fredrick C. Cross 16p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6904: A flight evaluation of methods for predicting vortex wake effects on trailing aircraft by Glenn H. Robinson 58p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6905: Lateral stability and control derivatives of a jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation by Russell V. Parrish 51p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6906: Simulation study of the lift roll coupling problem for hovering vtol aircraft by Robert A. Jacobsen 14p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6907: Turbulent boundary layer velocity profiles on a nonadibatic flat plate at mach number 6.5 by Earl R. Keener 43p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6908: Effects of wall cooling and angle of attack on boundary layer tansition on sharp cones at M = 7.4 by George G. Mateer 10p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-6909: Dynamic stsbility derivatives at angles of attack from 5 degree to 90 degree for a variable sweep fighter configuration with twin vertical tails by Sue B. Grafton 49p |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
