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Decade: 1940-1949

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Ditching Investigation of a 1/18-Scale Model of the North American B-45 Airplane

Ditching Investigation of a 1/18-Scale Model of the North American B-45 Airplane

Flight Test of the Aerojet 7KS-6000 T-27 Jato Rocket Motor

Flight Test of the Aerojet 7KS-6000 T-27 Jato Rocket Motor

A free-flight technique for measuring damping in roll by use of rocket-powered models and some initial results for rectangular wings

A free-flight technique for measuring damping in roll by use of rocket-powered models and some initial results for rectangular wings

Comparison of effectiveness of coordinated turns and level sideslips for correcting lateral displacement during landing approaches

Comparison of effectiveness of coordinated turns and level sideslips for correcting lateral displacement during landing approaches

Low-speed investigation of deflectable wing-tip ailerons on an untapered 45 degrees sweptback semispan wing with and without an end plate

Low-speed investigation of deflectable wing-tip ailerons on an untapered 45 degrees sweptback semispan wing with and without an end plate

Preliminary investigation of a variable mass-flow supersonic nose inlet

Preliminary investigation of a variable mass-flow supersonic nose inlet

Comparative tests of the rolling effectiveness of constant-chord, full-delta, and half-delta ailerons on delta wings at transonic and supersonic speeds

Comparative tests of the rolling effectiveness of constant-chord, full-delta, and half-delta ailerons on delta wings at transonic and supersonic speeds

Experimental investigation at supersonic speeds of side scoops employing boundary-layer suction

Experimental investigation at supersonic speeds of side scoops employing boundary-layer suction

The effects of scale and test technique on the validity of small-scale measurements of the aerodynamic characteristics of a wing with the leading edge swept back 63 degrees

The effects of scale and test technique on the validity of small-scale measurements of the aerodynamic characteristics of a wing with the leading edge swept back 63 degrees

An empirical criterion for fin stabilizing jettisonable nose sections of airplanes

An empirical criterion for fin stabilizing jettisonable nose sections of airplanes

Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel V : static longitudinal stability and control throughout the subsonic speed range of a semispan model of a supersonic airplane

Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel V : static longitudinal stability and control throughout the subsonic speed range of a semispan model of a supersonic airplane

Full-Scale Hydrodynamic Evaluation of a Modified Navy J4F-2 Amphibian with a 0.425-Scale XP5M-1 Hull Bottom. TED No. NACA DE325

Full-Scale Hydrodynamic Evaluation of a Modified Navy J4F-2 Amphibian with a 0.425-Scale XP5M-1 Hull Bottom. TED No. NACA DE325

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effects at subsonic speeds of a constant-chord elevon on a wing cambered and twisted for a uniform load at a lift coefficient of 0.25

Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : effects at subsonic speeds of a constant-chord elevon on a wing cambered and twisted for a uniform load at a lift coefficient of 0.25

Investigation of altitude performance of AN-F-58 fuels in annular combustor of J34-WE-22 engine

Investigation of altitude performance of AN-F-58 fuels in annular combustor of J34-WE-22 engine

Survey of two-dimensional data on pitching-moment changes near maximum lift caused by deflection of high-lift devices

Survey of two-dimensional data on pitching-moment changes near maximum lift caused by deflection of high-lift devices

Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).

Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6).

Analysis of means of improving the uncontrolled lateral motions of personal airplanes

Analysis of means of improving the uncontrolled lateral motions of personal airplanes

Effect of airfoil section and tip tanks on the aerodynamic characteristics at high subsonic speeds of an unswept wing of aspect ratio 5.16 and taper ratio 0.61

Effect of airfoil section and tip tanks on the aerodynamic characteristics at high subsonic speeds of an unswept wing of aspect ratio 5.16 and taper ratio 0.61

Experimental investigation of flutter of a propeller with Clark Y section operating at zero forward velocity at positive and negative blade- angle settings

Experimental investigation of flutter of a propeller with Clark Y section operating at zero forward velocity at positive and negative blade- angle settings

Investigation of Christy Titanium Deposit, Hot Spring County, Arkansas

Investigation of Christy Titanium Deposit, Hot Spring County, Arkansas

Investigation of Magnet Cove Rutile Deposit, Hot Spring County, Arkansas

Investigation of Magnet Cove Rutile Deposit, Hot Spring County, Arkansas

Investigation of the Huber-Rydalch Manganese Deposits, Tooele County, Utah

Investigation of the Huber-Rydalch Manganese Deposits, Tooele County, Utah

Investigation of the Yellow Pine Zinc-Lead Mine, Clark County, Nevada

Investigation of the Yellow Pine Zinc-Lead Mine, Clark County, Nevada

Landing Procedure in Model Ditching Tests of Bf 109

Landing Procedure in Model Ditching Tests of Bf 109

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