000			03083nam a22002057a 4500
005			20200219095507.0
008			200214b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
082			_aNASA TN _bD1821-1830
100			_aReed, Wilmer H.
110			_aNASA Washington
245			_aDynamic response of rising and falling balloon wind sensors with application to estimates of wind loads on launch vehicles _cWilmer H. Reed III
260			_aWashington _bNASA _c1963
300			_avarious pagings
440			_aNASA Technical Report
505			_aNASA 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			_aNASA Technical Report _aNASA Report _xNASA 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 _xNASA 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; _xNASA 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; _xNASA TN D- 1825 : Gas chromatographic measurement of trace contaminants in a simulated space cabin _xNASA TN D- 1826 : Preliminary flight evaluation of two unpowered manned paragliders; _xNASA TN D- 1827 : Fixed-base-simulator evaluation of a pilot's terrain-following display with various modes of presenting information; _xNASA TN D- 1828 : Theoretical investigation of the slideout dynamics of a vehicle equipped with a tricycle skid-type landing-gear system; _xNASA TN D- 1829 : Performance analysis of high-energy chemical stages for interplanetary missions; _xNASA TN D- 1830 : The significance of atmospheric ballistics in rocket technology;
942			_cTR
999			_c561357 _d561357