| 000 -LEADER |
|---|
| fixed length control field |
02265nam a2200301 4500 |
| 003 - CONTROL NUMBER IDENTIFIER |
|---|
| control field |
OSt |
| 005 - DATE AND TIME OF LATEST TRANSACTION |
|---|
| control field |
20220816134642.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION |
|---|
| fixed length control field |
220711b 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 D 171-180] |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) |
|---|
| 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-171: Calculated effective thermal conductivities of honeycomb sandwich panels by Robert T. Swann 24p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-172: Application of rate tempratures to tensile data for magnesium alloys and a relation between the larson miller constant and the activation energy by Charles R. Manning 23p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-173: Flight investigations of automatic stabilization of an airplane having static longitudinal instability by Walter R. Russel 32p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-174: Reflection Characteristics of artificial satellites constructed in the form of inflated polyhedrons by Archibald R. Sinclair 9p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-175: Dynamic model investigation of the damping of flapwise bending modes of two blade rotors in hovering and a comparision with quasi static and unsteady aerodynamic theories by Milton A. Silveria 30p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-176: Working charts for rapid prediction of force and pressure coefficients on arbitrary bodies of revolution by use of newtonian concepts by Robert W. Rainey 36p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-177: Jet effects of longitudinal trim of an airplane configuration measured at mach numbers between 1.2 and 1.8 by Robert F. Peck 17p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-178: Flutter investigation of a true speed dynamic model with various tip tank configurations by John L. Sewall 80p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-179: Measurements of pressure and local heat transfer on a 20 degree cone angles of attack upto 20 degree by Jerome D. Julius 28p |
| 500 ## - GENERAL NOTE |
|---|
| General note |
NASA TN D-180: Hydrodynamic characteristics of a planning surface with convex longitudinal curvature and an angle of dead rise of 20 degree by Elmo J. Mottard 27p |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM |
|---|
| Topical Term |
Hydrdynamic |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) |
|---|
| Koha item type |
Technical Report |
