Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles
By: Reed, Wilmer H | NASA Washington.
Material type:
BookSeries: NASA Technical Report. Publisher: Washington NASA 1963Description: various pagings.Subject(s): NASA Technical Report NASA Report -- 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 technologyDDC classification: NASA TN | D1821-1830 | Item type | Current location | Collection | Call number | Status | Date due | Barcode | Item holds |
|---|---|---|---|---|---|---|---|
Technical Report
|
PK Kelkar Library, IIT Kanpur | COMPACT STORAGE (BASEMENT) | NASA TN D 1821-1830 (Browse shelf) | Not for loan | 65574 NASA TN D 1821 |
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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;
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