Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles (Record no. 561357)
[ view plain ]
| 000 -LEADER | |
|---|---|
| fixed length control field | 03083nam a22002057a 4500 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20200219095507.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 200214b 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 |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | NASA TN |
| Item number | D1821-1830 |
| 100 ## - MAIN ENTRY--AUTHOR NAME | |
| Personal name | Reed, Wilmer H. |
| 110 ## - MAIN ENTRY--CORPORATE NAME | |
| Corporate name or jurisdiction name as entry element | NASA Washington |
| 245 ## - TITLE STATEMENT | |
| Title | Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles |
| Statement of responsibility, etc | Wilmer H. Reed III |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
| Place of publication | Washington |
| Name of publisher | NASA |
| Year of publication | 1963 |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | various pagings |
| 440 ## - SERIES STATEMENT/ADDED ENTRY--TITLE | |
| Title | NASA Technical Report |
| 505 ## - FORMATTED CONTENTS NOTE | |
| Formatted contents note | NASA TN D-1822 : Low-subsonic measurements of static and dynamic stability derivatives of six flat-plate wings having leading-edge sweep angles of 70 to 80 by Robert E. Shanks; NASA TN D-1823 : Aerodynamic characteristics in pitch at a mach number of 2.01 of several wing-body combinations with wedge-shaped bodies located above and below A 54.5 swept delta wing by Odell A. Morris; NASA TN D- 1824 : Use of aerodynamic parameters from nonlinear theory in modified-strip-analysis flutter calculations for finite-soan wings at supersonic speeds by E. Carson Yates; NASA TN D- 1825 : Gas chromatographic measurement of trace contaminants in a simulated space cabin; NASA TN D- 1826 : Preliminary flight evaluation of two unpowered manned paragliders; NASA TN D- 1827 : Fixed-base-simulator evaluation of a pilot's terrain-following display with various modes of presenting information; NASA TN D- 1828 : Theoretical investigation of the slideout dynamics of a vehicle equipped with a tricycle skid-type landing-gear system; NASA TN D- 1829 : Performance analysis of high-energy chemical stages for interplanetary missions; NASA TN D- 1830 : The significance of atmospheric ballistics in rocket technology; |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical Term | NASA Technical Report |
| -- | NASA Report |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | Technical Report |
| Withdrawn status | Lost status | Damaged status | Not for loan | Collection code | Permanent Location | Current Location | Date acquired | Full call number | Accession Number | Koha item type |
|---|---|---|---|---|---|---|---|---|---|---|
| COMPACT STORAGE (BASEMENT) | PK Kelkar Library, IIT Kanpur | PK Kelkar Library, IIT Kanpur | 2020-02-19 | NASA TN D 1821-1830 | 65574 NASA TN D 1821 | Technical Report |