PKK Library Search for 'au:"ROLLS,L STEWART"'

AN INVESTIGATION OF THE DRAG CHARACTERISTICS OF A TAILLESS DELTA-WING AIRPLANE FLIGHT, INCLUDING COMPARISON WITH WIND-TUNNEL DATA

By Rolls,L Stewart. Nasa, Washington, D.C. 1958 . 34 , Bound With Nasa Memo10-1-58a-10-7-58a.Lack No Nasa Memo10-2-58a,10-7-58a

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A FLIGHT DETERMINATION OF THE ATTITUDE CONTROL POWER AND DAMPING REQUIREMENTS FOR A VISUAL HOVERING TASK IN THE VARIABLE STABILITY AND CONTROL X-14A RESEARCH VEHICLE

By Rolls,L Stewart. Nasa, Washington, D.C. 1962 . 20 , Bound With Nasa Tn D-1321-1327,1329-1330

Place Hold on A FLIGHT DETERMINATION OF THE ATTITUDE CONTROL POWER AND DAMPING REQUIREMENTS FOR A VISUAL HOVERING TASK IN THE VARIABLE STABILITY AND CONTROL X-14A RESEARCH VEHICLE

FLIGHT EVALUATION OF TIP-TURBINE-DRIVEN FANS FOR LATERAL CONTROL IN A HOVERING VTOL AIRCRAFT

By ROLLS,L STEWART. NASA, WASHINGTON, D.C. 1969 . ,16,,,,,, , Bound with NASA TN D-5492-98 Lack No.5494,5496

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Flight investigation of the aerodynamic properties of an ogee wing. [TN D 3071-TN D 3080]

By Rolls, L. Stewart. Washington, D. C. NASA 1965 . 21p , TR63214{a} :[TN D-3072] Experimental profiles of velocity components and Radial pressure distributions in a vortex contained in ashort cylindrical chamber by Joseph M. Savino and Edward G. Keshock TR63214{b} : [TN D-3073] Elevated -temperature tensile properaties of alloyed tungsten fiber composites by Donald W. Petrasek TR63214{c} : [TN D-3074] An investigation of heat transfer within regions separated flow at a mach number of 6.0 by Paul F. Holloway , James R. Sterrett, and Helen S. Creekmore TR63214{d} : [TN D-3075] Fatigue of rene 41 under constant -and random-amplitude loading at room and elevated temperatures by Edward P. Phillips TR 63214{e} : [TN D-3076] Calibration of conical pressure probes for determination of local flow conditions at mach numbers from 3 to 6 by John D. Norris TR63214{F} : [TN D-3077] Super sonic flutter of a thermally stressed flat panel with uniform edge loges by Harry G. Schaeffer and Walter L. Heard jr TR63214{g} : [TN D-3078] Computation of general planetary perturbations by Lloyd carpenter TR 63214{h} : [TN D-3079] Comparison of phase- coherent and non-phase-coherent coded communications by J.P. Strong and T.V.Saliga TR63321{i} : [TN D-3080] Analysis of chugging in liquid-bipropellant rocket engines using propellants with different vaporization rates by Leon M. Wenzel and John R. Szuch

Place Hold on Flight investigation of the aerodynamic properties of an ogee wing. [TN D 3071-TN D 3080]

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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