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       - / .- Washington, D. C.: National Aeronautics and Space Administrtion, 1972 .- ( National Aeronautics and Space Administrtion NASA Technical Note
NASA TN D-6900: Effect of stabilization on vtol aircraft in hovering flight by Richard K. Greif 19p NASA TN D-6901: Atmospheric electricity criteria guidelines for use in aerospace vehicle development by Glenn E. Daniels 18p NASA TN D-6902: The interaction of moderately strong shock waves with thick perforated walls of low porosity by Daniel J. Grant 69p NASA TN D-6903: An ethological study of phthalate self contamination of spacecraft and contamination from their earthly environs by Fredrick C. Cross 16p NASA TN D-6904: A flight evaluation of methods for predicting vortex wake effects on trailing aircraft by Glenn H. Robinson 58p NASA 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 NASA TN D-6906: Simulation study of the lift roll coupling problem for hovering vtol aircraft by Robert A. Jacobsen 14p NASA TN D-6907: Turbulent boundary layer velocity profiles on a nonadibatic flat plate at mach number 6.5 by Earl R. Keener 43p NASA 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 NASA 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
Copy Details:
Acc. No.: 101280, Full Call No.: , Item type: Technical Report , Location: COMPACT STORAGE (BASEMENT), NASA TN D 6900-6909
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