PKK Library Search for 'au:"Innis, Robert C. "'

FLIGHT-DETERMINED AERODYNAMIC PROPERTIES OF A JET-AUGMENTED, AUXILIARY-FLAP, DIRECT-LIFT-CONTROL SYSTEM INCLUDING CORRELATION WITH WIND-TUNNEL RESULTS

By Rolls,Stewart, Cook,Anthony M. Nasa, Washington, D.C. 1969 . 39 , Bound With Nasa Tn D-5111-30

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A FLIGHT EXAMINATION OF OPEARTING PROBLEMS OF V/STOL AIRCRAFT IN STOL-TYPE LANDING AND APPROACH.

By Innis,Robert C. Nasa, Washington, D.C. 1961 . 43 , Bound With: Nasa Tn D-861,863-870.

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A FLIGHT AND SIMULATOR STUDY OF DIRECTIONAL AUGMENTATION CRITERIA FOR A FOUR-PROPELLERED STOL AIRPLANE.

By Quigley,Hervey C,Innis,Robert C. National Aeronautics And Space Administration, Washington, D.C. . 39 , Bound With Nasa Tn D-3901-3908,3910

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A SIMULATOR AND FLIGHT STUDY OF YAW COUPLING IN TURNING MANEUVERS OF LARGE TRANSPORT AIRCRAFT.

By Mcneill,Walter E. National Aeronautics And Space Administration, Washington, D.C. . 37 , Bound With Nasa Tn D-3901-3909

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A FLIGHT EVALUATION OF A VTOL JET TRANSPORT UNDER VISUAL AND SIMULATED INSTRUMENT CONDITIONS

By Holzbauser,Curt A,Morellon,Samuel A. Nasa, Washington, D.C. 1972 . 88 , Bound With Nasa Tn D-6750-6753, 6755-6759

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NASA Memorandum [NASA MEMO 4-15-59A]: A flight investigation of the low-speed handling qualities of a tailless delta-wing fighter airplane

Washington NASA. 1959 . 33p , Bound together NASA MEMO 4-14-59A to 4-27-59A Lack No.4-16 to 4-17, 4-22 to 4-25 | Bound vol. Acc. No. 102439 contains Acc. No. TR11609 to TR11615

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FLIGHT TESTS UNDER IFR WITH AN STOL TRANSPORT AIRCRAFT

By Innis,Robert C,Holzhauser,Curt A. Nasa, Washington, D.C. 1968 . 61 , Bound With Nasa Tn D-4931-38,4940

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A RESTRAINT SYSTEM ENABLING PILOT CONTROL UNDER MODERTELY HIGH ACCEKERATION IN A VARIED ACCELERATION FIELD .

By Samedal,Captain Harald A,Stinnett,Glen W. Nasa, Washington, D.C. 1960 . 19 , Bound With Nasa Tn D-92-100.

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FLIGHT INVESTIGATION OF THE LOW-SPEED CHARCTERISTICS OF A 45 DEGREE SWEPT-WING FIGHTER-TYPE AIRPLANE WITH BLOWING BOUNADRY-LAYER CONTROL APPLIED TO THE LEADING- AND TRAILING-EDGE FLAPS.

By Quigley,Hervey C,Anderson,Seth B. Nasa, Washington, D.C. 1960 . 44 , Bound With Nasa Tn D-322-330.

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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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NASA TN [D-4141]

By Feistel, Terrell W.. Washington National Aeronautics and Space Administration 1967 . 37p , Technical Note D-4141-4150 Bound Vol. No.86777; Contents: TR-9007-9015

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