NASA TN / D1821-1830
Reed, Wilmer H.
Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles / Wilmer H. Reed III .- Washington: NASA, 1963 .- various pagings. .- ( NASA Technical Report
Subject Headings:
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 technology;
Copy Details:
Acc. No.: 65574 NASA TN D 1821, Full Call No.: NASA TN D 1821-1830, Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT),
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Reed, Wilmer H.
Dynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles / Wilmer H. Reed III .- Washington: NASA, 1963 .- various pagings. .- ( NASA Technical Report
Subject Headings:
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 technology;
Copy Details:
Acc. No.: 65574 NASA TN D 1821, Full Call No.: NASA TN D 1821-1830, Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT),
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