Technical Report Archive and Image Library (TRAIL) - 16 Matching Results

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Primary view of Aerodynamic load distribution over a 45 degree swept wing having a spoiler-slot-deflector aileron and other spoiler ailerons for Mach numbers from 0.60 to 1.03
West, F. E., Jr.; Whitcomb, Charles F. & Schmeer, James W.
December 5, 1957
Primary view of Experimental investigation of the transonic and supersonic flutter characteristics of the upper and lower vertical tails of an air-to-ground missile
Hanson, P. W. & Rainey, A. G.
June 5, 1957
Primary view of Flight Investigation of the Transonic Longitudinal and Lateral Handling Qualities of the Douglas X-3 Research Airplane
Fischel, Jack; Holleman, Euclid C. & Tremant, Robert A.
December 5, 1957
Primary view of Investigation at High Subsonic Speeds of the Use of Low Auxiliary Tail Surfaces Having Dihedral to Improve the Longitudinal and Directional Stability of a T-Tail Model at High Lift
Sleeman, William C., Jr.
December 5, 1957
Primary view of Investigation of Ejection Release Characteristics of Bluff TX-28 and Turnabout TX-28 Stores From a 1/17-Scale Simulated Bomb Bay of the Republic F-105 Airplane at Mach Numbers of 1.39 and 1.98 : Coord. No. AF-222
Lee, John B.
February 5, 1957
Primary view of NACA Conference on Aircraft Loads, Structures, and Flutter
unknown creator
March 5, 1957
Primary view of Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure distribution measurements on an inboard aileron
Runckel, Jack F. & Hieser, Gerald
December 5, 1957
Primary view of Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine 4: over-all performance of first-stage turbine with reduced-chord rotor blades at inlet conditions of 35 inches of mercury absolute and 700 R
Schum, Harold J.
July 5, 1957
Primary view of Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine 5: effect of inlet pressure on over-all performance at design speed and inlet temperature of 700 degrees R
Schum, Harold J.
July 5, 1957
Primary view of Relation of Turbojet and Ramjet Combustion Efficiency to Second-Order Reaction Kinetics and Fundamental Flame Speed
Childs, J. Howard; Reynolds, Thaine W. & Graves, Charles C.
August 5, 1957
Primary view of Results of an investigation at high subsonic speeds to determine lateral-control and hinge-moment characteristics of a spoiler-slot-deflector configuration on a 35 degree sweptback wing
Hammond, Alexander D. & Brown, Albert E.
June 5, 1957
Primary view of Static Longitudinal and Lateral Stability Parameters of Three Flared-Skirt Two-Stage Missile Configurations at a Mach Number of 6.86
Penland, Jim A. & Carroll, C. Maria
June 5, 1957
Primary view of Transonic flutter investigation of a cantilevered, aspect-ratio-4, 45 degree sweptback, untapered wing with three different pylon-mounted external store configurations
Ruhlin, Charles L. & Boswinkle, Robert W., Jr.
July 5, 1957
Primary view of A variational theorem for creep with applications to plates and columns
Sanders, J. Lyell, Jr.; McComb, Harvey G., Jr. & Schlechte, Floyd R.
March 5, 1957
Primary view of Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with blowing flaps and leading-edge slats
James, Harry A. & Maki, Ralph L.
July 5, 1957
Primary view of Wind-tunnel Tests of the Static Longitudinal Characteristics at Low Speed of a Swept-wing Airplane With Blowing Flaps and Leading-edge Slats
James, H. A. & Maki, R. L.
April 5, 1957