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Partner: UNT Libraries Government Documents Department

Decade: 1950-1959

Year: 1955

Results 121 - 144 of 846

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The wave drag of arbitrary configurations in linearized flow as determined by areas and forces in oblique planes

The wave drag of arbitrary configurations in linearized flow as determined by areas and forces in oblique planes

Effect of rotor leading-edge sweepback on performance of a transonic turbine

Effect of rotor leading-edge sweepback on performance of a transonic turbine

Investigation of boattail and base pressures of twin-jet afterbodies at Mach number 1.91

Investigation of boattail and base pressures of twin-jet afterbodies at Mach number 1.91

Flight measurements of the lateral response characteristics of the Convair XF-92A delta-wing airplane

Flight measurements of the lateral response characteristics of the Convair XF-92A delta-wing airplane

Ditching investigation of a 1/25-scale model of a 255,000-pound transport airplane

Ditching investigation of a 1/25-scale model of a 255,000-pound transport airplane

Effect of surface-active additives on physical properties of slurries of vapor-process magnesium

Effect of surface-active additives on physical properties of slurries of vapor-process magnesium

An investigation of loads on ailerons at transonic speeds

An investigation of loads on ailerons at transonic speeds

Wing pressure distributions over the lift range of the Convair XF-92A delta-wing airplane at subsonic and transonic speeds

Wing pressure distributions over the lift range of the Convair XF-92A delta-wing airplane at subsonic and transonic speeds

Free-flight investigation to determine some effects of tail damping and wing-tail interference on the rolling effectiveness of inboard and outboard ailerons on an untapered sweptback wing

Free-flight investigation to determine some effects of tail damping and wing-tail interference on the rolling effectiveness of inboard and outboard ailerons on an untapered sweptback wing

Study of some effects of structural flexibility on the longitudinal motions and loads as obtained from flight measurements of a swept-wing bomber

Study of some effects of structural flexibility on the longitudinal motions and loads as obtained from flight measurements of a swept-wing bomber

Effect of dissolved oxygen on the filterability of jet fuels for temperatures between 300 degrees and 400 degrees F

Effect of dissolved oxygen on the filterability of jet fuels for temperatures between 300 degrees and 400 degrees F

Low-speed study of the effects of frequency on the stability derivatives of wings oscillating in yaw with particular reference to high angle of attack conditions

Low-speed study of the effects of frequency on the stability derivatives of wings oscillating in yaw with particular reference to high angle of attack conditions

Flight investigation of a roll-stabilized ram-jet test vehicle over a mach number range of 2.3 to 2.7

Flight investigation of a roll-stabilized ram-jet test vehicle over a mach number range of 2.3 to 2.7

Simplified procedures for estimating flap-control loads at supersonic speeds

Simplified procedures for estimating flap-control loads at supersonic speeds

Statistical measurements of landing contact conditions of the Boeing B-47 airplane

Statistical measurements of landing contact conditions of the Boeing B-47 airplane

Component operating trends during acceleration and deceleration of two hypothetical two-spool turbojet engines

Component operating trends during acceleration and deceleration of two hypothetical two-spool turbojet engines

Preliminary results of an investigation at transonic speeds to determine the effects of a heated propulsive jet on the drag characteristics of a related series of afterbodies

Preliminary results of an investigation at transonic speeds to determine the effects of a heated propulsive jet on the drag characteristics of a related series of afterbodies

Investigation at supersonic speeds of external-drag effects and pumping characteristics of a short ejector

Investigation at supersonic speeds of external-drag effects and pumping characteristics of a short ejector

Experimental rocket performance with 15 percent fluorine - 85 percent oxygen and JP4

Experimental rocket performance with 15 percent fluorine - 85 percent oxygen and JP4

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections III : comparison of blade-element performance with three levels of solidity

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections III : comparison of blade-element performance with three levels of solidity

A correlation of airfoil section data with the aerodynamic loads measured on a 45 degree sweptback wing model at subsonic Mach numbers

A correlation of airfoil section data with the aerodynamic loads measured on a 45 degree sweptback wing model at subsonic Mach numbers

Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303

Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303

Drag near zero lift of a 1/7-scale model of the Convair B-58 external store as measured in free flight between Mach numbers of 0.8 and 2.45

Drag near zero lift of a 1/7-scale model of the Convair B-58 external store as measured in free flight between Mach numbers of 0.8 and 2.45

Effect of ejector performance of varying diameter ratio by simulated iris flaps

Effect of ejector performance of varying diameter ratio by simulated iris flaps

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