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Investigation of Downwash, Sidewash, and Mach Number Distribution Behind a Rectangular Wing at a Mach Number of 2.41

Free-Flight Investigation of the Static and Dynamic Longitudinal Stability Characteristics of 1/3.7-Scale Rocket-Powered Models of the Bell MX-776A

Theoretical Investigation of a Proportional-Plus-Flicker Automatic Pilot

Tests of the Northrop XSSM-A-3 Missile in the Ames 40- by 80-Foot Wind Tunnel: Wing Modifications

High-Subsonic Performance Characteristics and Boundary-Layer Investigations of a 12 10-Inch-Inlet-Diameter Conical Diffuser

Free-Space Oscillating Pressures Near the Tips of Rotating Propellers

The Gas Kinetics of Very High Flight Speeds

Positioning Investigation of Single Slotted Flaps on a 47.7 Degrees Sweptback Wing at Reynolds Numbers of 4.0 X 10(Exp 6) and 6.0 X 10(Exp 6)

Preliminary Empirical Design Requirements for the Prevention of Tumbling of Airplanes Having No Horizontal Tails

Generalization of Boundary-Layer Momentum-Integral Equations to Three-Dimensional Flows Including Those of Rotating System

Damping in Roll of Rectangular Wings of Several Aspect Ratios and Naca 65a-Series Airfoil Sections of Several Thickness Ratios at Transonic and Supersonic Speeds as Determined With Rocket-Powered Models

Investigation of the NACA 3-(3)(05)-05 Eight-Blade Dual-Rotating Propeller at Forward Mach Numbers to 0.925

Investigation of the NACA 4-(4)(06)-057-45a and NACA 4-(4)(06)-57-45b Two-Blade Swept Propellers at Forward Mach Numbers to 0.925

Flight Measurements of Base Pressure on Bodies of Revolution With and Without Simulated Rocket Chambers

Evaluation of Several Adhesives and Processes for Bonding Sandwich Constructions of Aluminum Facings on Paper Honeycomb Core

Aerodynamic Characteristics of Damping Screens

Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section

Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7

The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel

An analysis of base pressure at supersonic velocities and comparison with experiment

Analysis of an induction blowdown supersonic tunnel

Analysis for Control Application of Dynamic Characteristics of Turbojet Engine With Tail-Pipe Burning

Investigation of Boundary-layer Control to Improve the Lift and Drag Characteristics of the NACA 65₂-415 Airfoil Section with Double Slotted and Plain Flaps

Temperature distribution in internally heated walls of heat exchangers composed of noncircular flow passages

Compressive strength of flanges

X-Ray Diffraction by Bent Crystal Lamellae

Flight determination of the drag and pressure recovery of an NACA 1-40-250 nose inlet at Mach numbers from 0.9 to 1.8

Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range

Comparison of NACA 65-series compressor-blade pressure distributions and performance in a rotor and in cascade

Aerodynamic characteristics of a leading-edge slat on a 35 degree swept-back wing for Mach numbers from 0.30 to 0.88

NACA VGH recorder

An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47©� sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel

Average Outside-Surface Heat-Transfer Coefficients and Velocity Distributions for Heated and Cooled Impulse Turbine Blades in Static Cascades

Flight Performance of a Jet Power Plant, III, operating characteristics of a jet power plant as a function of altitude

Strain-Gage Measurements of Buffeting Loads on a Jet-Powered Bomber Airplane

Matching Characteristics of J35-A-23 Compressor and Two-stage Turbine

Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds: Triangular Wing of Aspect Ratio 2 with NACA 0005-63 Thickness Distribution, Cambered and Twisted for a Trapezoidal Span Load Distribution

Investigation of Surge Characteristics of XJ34-WE-32 Turbojet Engine

Ditching Investigation of a 1/24-Scale Model of the Douglas C-124 Airplane

Flight Instrument for Measurement of Liquid-Water Content in Clouds at Temperatures Above and Below Freezing

An Instrument Employing a Coronal Discharge for the Determination of Droplet-Size Distribution in Clouds

Measurement of distortion in second experimental control rod for argonne naval reactor with constant transverse temperature gradient and uniform longitudinal temperature distribution

X-Ray Diffraction Study of the Internal Structure of Supercooled Water

Spark Ignition of Flowing Gases. 2: Effect of Electrode Parameters on Energy Required to Ignite a Propane-Air Mixture

Theoretical Investigation of Submerged Inlets at Low Speeds

Analysis of the Liquid-metal Turbojet Cycle for Propulsion of Nuclear Powered Aircraft

Experimental Investigation of Air-Cooled Turbine Blades in Turbojet Engine. 7: Rotor-Blade Fabrication Procedures

Effectiveness of Thermal-Pneumatic Airfoil-Ice-Protection System

Heat delivery in a compressible flow and applications to hot-wire anemometry

Analytical method for determining performance of turbojet-engine tail-pipe heat exchangers


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