000			02048nam a2200289 4500
003			OSt
005			20220907120702.0
008			220907b xxu||||| |||| 00| 0 eng d
040			_cIIT Kanpur
041			_aeng
110			_aWashington: National Aeronautics and Space Administrtion
245			_a-
260			_aWashington, D. C. _bNational Aeronautics and Space Administrtion _c1972
440			_aNational Aeronautics and Space Administrtion
440			_aNASA Technical Note
500			_aNASA TN D-6900: Effect of stabilization on vtol aircraft in hovering flight by Richard K. Greif 19p
500			_aNASA TN D-6901: Atmospheric electricity criteria guidelines for use in aerospace vehicle development by Glenn E. Daniels 18p
500			_aNASA TN D-6902: The interaction of moderately strong shock waves with thick perforated walls of low porosity by Daniel J. Grant 69p
500			_aNASA TN D-6903: An ethological study of phthalate self contamination of spacecraft and contamination from their earthly environs by Fredrick C. Cross 16p
500			_aNASA TN D-6904: A flight evaluation of methods for predicting vortex wake effects on trailing aircraft by Glenn H. Robinson 58p
500			_aNASA TN D-6905: Lateral stability and control derivatives of a jet fighter airplane extracted from flight test data by utilizing maximum likelihood estimation by Russell V. Parrish 51p
500			_aNASA TN D-6906: Simulation study of the lift roll coupling problem for hovering vtol aircraft by Robert A. Jacobsen 14p
500			_aNASA TN D-6907: Turbulent boundary layer velocity profiles on a nonadibatic flat plate at mach number 6.5 by Earl R. Keener 43p
500			_aNASA TN D-6908: Effects of wall cooling and angle of attack on boundary layer tansition on sharp cones at M = 7.4 by George G. Mateer 10p
500			_aNASA TN D-6909: Dynamic stsbility derivatives at angles of attack from 5 degree to 90 degree for a variable sweep fighter configuration with twin vertical tails by Sue B. Grafton 49p
942			_cTR
999			_c566089 _d566089