FLOW-FIELD AND DRAG CHARACTERISTICS OF SEVERAL BOUNDARY-LAYER TRIPPING ELEMENTS IN HYPERSONIC FLOW

By Whitehead,Allen H. Nasa, Washington, D.C. 1969 . 38 , Bound With Nasa Tn D-5451-53,5455-70

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Effect of body cross section and width-height ratio on performance of bodies and delta-win-body combinations at mach 6.9 [NASA TN D-2886]

By Whitehead, Allen H. . . 25p

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NASA Technical Note [D-2701-2710]

Washington National Aeronautics and Space Administration (NASA) 1965 , NASA TN D-2701: Effects of Lateral control, characteristics on hovering: jet lift vtol aircraft/ by L. Stewart Rolls, Fred J. Drinkwater III and Robert C. Innis | NASA TN D-2702: Impact of V / STOL aircraft on instrument weather operations/ John P. Reeder | NASA TN D-2703: Description and initial calibration of the langley 12-inch Hypersonic ceramic-heated tunnel/ Louis E. Clark | NASA TN D-2704: Hemispherical spectral emittance of ablation chars, carbon, and zirconia to 3700 degree K / by R. Gale Wilson | NASA TN D-2705: results of USAF-NASA-FAA flight program to study community responses to sonic booms in the greater St. Louis Area/ by Charles W. Nixon, Harvey H. Hubbard | NASA TN D-2706: Effect of surface emittance on turbulent skin friction at supersonic and low hypersonic speeds/ Jerry M. Allen and K. R. Czarnecki | NASA TN D-2707: Fixed- base simulator study of piloted entry into the earth's atmosphere at parabolic velocity/ by Martin T. Moul and Albert A. Schy | NASA TN D-2708: Study of pressure and heat transfer over an 80 degree sweep slab delta wing in hypersonic flow/ Allen H. Whitehead and James C. Dunavant | NASA TN D-2709: Effect of first-stage geometry on aerdynamic characteristics in pitch of two-stage rocket vehicles from mach 1.57 to 2.86/ by William A. Corlett and Celia S. Richardson | NASA TN D-2710: Effect of combined linear and oscillatory acceleration on pilot attitude-control capabilities/by Constantine B. Dolkas and John D. Stewart

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FLOW-FIELD AND DRAG CHARACTERISTICS OF SEVERAL BOUNDARY-LAYER TRIPPING ELEMENTS IN HYPERSONIC FLOW

Effect of body cross section and width-height ratio on performance of bodies and delta-win-body combinations at mach 6.9 [NASA TN D-2886]

NASA Technical Note [D-2701-2710]