TRAIL - Technical Report Archive and Image Library

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

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

Hydrodynamic Properties of Planing Surfaces and Flying Boats

The Boundary Layers in Fluids with Little Friction

The Effect of the Inlet Mach Number and Inlet-Boundary-Layer Thickness on the Performance of a 23 Degree Conical-Diffuser-Tail-Pipe Combination

Annual Report of the National Advisory Committee for Aeronautics (33rd). Administrative Report Including Technical Report Nos. 863 to 891

Dynamic Response of Control Servo System Installed in NAES-Equipped SB2C-5 Airplane (BuAer No. 83135)

Ditching Investigation of a 1/10-Scale Model of the Grumman F9F-2 Airplane, TED No. NACA DE 335

Ditching Investigation of a 1/15-Scale Model of the Convair-Liner Airplane

Ditching Investigation of a 1/14-Scale Model of the Northrop C-125 Airplane

Investigation of the Spin and Recovery Characteristics of a 0.057-Scale Model of the Modified Chance Vought XF7U-1 Airplane. TED No. NACA DE 311

Free-Spinning-Tunnel Investigation of a 1/24-Scale Model of the Grumman AF-2S, -2W Airplane

Free-Spinning-Tunnel Investigation of a 1/30-Scale Model of the Grumman XF10F-1 Airplane

Instrument for Measuring the Wall Shearing Stress of Turbulent Boundary Layers

Investigations of Lateral Stability of a Glide Bomb Using Automatic Control Having No Time Lag

Investigations of the Wall-Shearing Stress in Turbulent Boundary Layers

An Investigation of the Longitudinal Characteristics of the MX-656 Configuration Using Rocket-Propelled Models Preliminary Results at Mach Numbers from 0.65 to 1.25

Some Studies on the Flow of a Gas in the Region of Transition Through the Velocity of Sound

Theoretical Investigations on the Efficiency and the Conditions for the Realization of Jet Engines

Wind-Tunnel Investigation of a Full-Scale Model of the Hughes MX-904 Missile

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

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

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

NACA VGH recorder

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

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

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

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