Experimental investigation of two methods for reducing transonic drag of swept-wing and body combinations /

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

Experimental investigation of some aerodynamic effects of a gap between wing and body of a moderately slender wing-body combination at a Mach number of 1.4 /

Investigation of the effects of an airfoil section modification on the aerodynamic characteristics at subsonic and supersonic speeds of a thin swept wing of aspect ratio 3 in combination with a body /

Effects of flexibility on the longitudinal and lateral-directional response of a large airplane /

Experimental investigation at Mach numbers from 0 to 1.9 of trapezoidal and circular side inlets for a fighter-type airplane /

Load distribution on wings and wing-body combinations at high angles of attack and supersonic speeds /

Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98 /

Theoretical investigation of the effects of configuration changes on the center-of-pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transonic and supersonic speeds /

Drag and rolling-moment effectiveness of trailing-edge spoilers at Mach numbers 2.2 and 5.0 /

Aerodynamic principles for the design of jet-engine induction systems /

Flight investigation at transonic speeds of a model having a triangular wing of aspect ratio 2 /

Preliminary experimental investigation of a variable-area, variable-internal-contraction air inlet at Mach numbers between 1.42 and 2.44 /

Fuselage side inlets : a study of some factors affecting their performance and a comparison with nose inlets /

Effects of boundary-layer separation on normal force and center of pressure of a cone-cylinder model with a large base flare at Mach numbers from 3.00 to 6.28 /

Method for simulating the atmospheric entry of long-range ballistic missiles /

Application of Tchebichef form of harmonic analysis to the calculation of zero-lift wave drag of wing-body-tail combinations /

Effects of two trailing-edge controls on the aerodynamic characteristics of a rectangular wing and body combination at Mach numbers from 3.00 to 5.05 /

Force, moment, and pressure-distribution characteristics of rectangular wings at high angles of attack and supersonic speeds /

Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28 /

Effect of boundary-layer control and inlet lip shape on the performance on a twin-scoop air-induction system at Mach numbers from 0 to 1.9 /

Aircraft configurations developing high lift-drag ratios at high supersonic speeds /

Aerodynamics of missiles employing wings of very low aspect ratio /

Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds /

Problems of performance and heating of hypersonic vehicles /

Study of a symmetrical, circular, internal compression inlet /

Light diffusion through high-speed turbulent boundary layers /

Investigation of the use of area suction to increase the effectiveness of trailing-edge flaps of various spans on a wing of 45 degree sweepback and aspect ratio 6 /

Method of reducing heat transfer to blunt bodies by air injection /

Effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil section, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems /

Change with mass-flow ratio of the cowl pressure drag of normal-shock inlets at supersonic speeds /

Use of area suction for improving the longitudinal characteristics of a thin unswept wing-fuselage model with leading- and trailing-edge flaps /

Full-scale wind-tunnel tests of a 35 degree sweptback-wing airplane with high-velocity blowing over the trailing-edge flaps : longitudinal and lateral stability and control /

Simulator study of some longitudinal stability and control problems of a piloted aircraft in flights to extreme altitude and high speed /

Analysis of some parameters used in correlating blowing-type boundary-layer control data /

Motion of a ballistic missile angularly misaligned with the flight path upon entering the atmosphere and its effect upon aerodynamic heating, aerodynamic loads, and miss distance /

Measurements of boundary-layer transition at low speed on two bodies of revolution in a low-turbulence wind tunnel /

Wind-tunnel tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on the trailing-edge flaps of a 35 degree sweptback wing airplane /

Flight measurements of the low-speed characteristics of a 35 degree swept-wing airplane with blowing-type boundary-layer control in the trailing-edge flaps /

Subsonic lateral and longitudinal static stability characteristics up to large angles of sideslip for a triangular-wing airplane model having a ventral fin /

Large-scale wind-tunnel tests of an airplane model with a 45 degree sweptback wing of aspect ratio 2.8 with area suction applied to trailing-edge flaps and with several wing leading-edge modifications /

Investigation of the lift, drag, and static-stability characteristics of a triangular-wing airplane configuration at Mach numbers from 3.00 to 6.28 /

Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution /

Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0 /

Investigation of wing-body juncture interference effects at transonic speeds for several swept-wing and body combinations /

Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with slotted flaps, area suction flaps, and wing leading-edge devices /

Lateral-directional aerodynamic characteristics of several coplanar triple-body missile configurations at Mach numbers from 0.6 to 1.4 /

Leading-edge contours for thin swept wings : an analysis of low-and high-speed data /

Flight investigation of area-suction and blowing boundary-layer control on the trailing-edge flaps of a 35 degree swept-wing carrier-type airplane /

Air-borne target simulator for use with scope-presentation type fire-control systems /

Investigation of boundary-layer transition on flat-faced bodies of revolution at high supersonic speeds /

Analytical study of the comparative pitch-up behavior of several airplanes and correlation with pilot opinion /

Flight tests of an automatic interceptor system with a tracking radar modified to minimize the interaction between antenna and interceptor motions /

Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with blowing flaps and leading-edge slats /

Comparison of carrier approach speeds as determined from flight tests and from pilot-operated simulator studies /

Aerodynamic loads on tails at high angles and sideslip /

Investigation of axially symmetric flow over steps at transonic speeds with comparisons of estimated and experimental drag results /

Effects of target and missile characteristics on theoretical minimum miss distance for a beam-rider guidance system in the presence of noise /

Flight investigation of the low-speed characteristics of a 35° swept-wing airplane equipped with an area-suction ejector flap and vaious wing leading-edge devices /

Wing-body combinations with wings of very low aspect ratio at supersonic speeds /

Effects of a leading-edge slat and a trailing-edge split flap on the aerodynamic characteristics of a wing-fuselage combination having a nearly triangular wing of aspect ratio 2.9 at Mach numbers from 0.60 to 0.92 /

Use of a leading-edge area-suction flap and leading-edge modifications to improve the high-lift characteristics of an airplane model with a wing of 45 degree sweep and aspect ratio 2.8 /