Browse TRAIL Inventories

Flutter and oscillating air-force calculations for an airfoil in a two-dimensional supersonic flow

Effect of change in cross section upon stress distribution in circular shell-supported frames

Tests of a full-scale horizontal tail surface in the Langley 16-foot high-speed tunnel

Theoretical lift and drag of thin triangular wings at supersonic speeds

Thin oblique airfoils at supersonic speed

Comparison of measured and calculated stresses in built-up beams

An investigation of additional requirements for satisfactory elevator control characteristics

Langley full-scale-tunnel investigation of the fuselage boundary layer on a typical fighter airplane with a single liquid-cooled engine

Measurements of landing-gear forces and horizontal-tail loads in landing tests of a large bomber-type airplane

Investigation of the effect of a tip modification and thermal de-icing air flow on propeller performance

Tank Tests to Determine the Effect of Varying Design Parameters of Planing-Tail Hulls 1: Effect of Varying Length, Width, and Plan-Form Taper of Afterbody

The effect of simulated icing on propeller performance

Flight tests of an all-movable horizontal tail with geared unbalancing tabs on the Curtiss XP-42 airplane

Wing plan forms for high-speed flight

Boundary-layer-control tests of two wings in the Langley Propeller-Research Tunnel

Calculation of surface temperatures in steady supersonic flight

Bending-Torsion Flutter Calculations Modified by Subsonic Compressibility Corrections

The effects of various parameters on the load at which spray enters the propellers of a flying boat

Increasing the compressive strength of 24S-T aluminum-alloy sheet by flexure rolling

Experimental determination of the effects of dihedral, vertical-tail area, and lift coefficient on lateral stability and control characteristics

General tank tests of a 1/10-size model of the hull of the Boeing XPBB-1 flying boat - Langley Tank Model 175

Jet-boundary and plan-form corrections for partial-span models with reflection plane, end plate, or no end plate in a closed circular wind tunnel

Pressure distribution over a plug-type spoiler-slot aileron on a tapered wing with full span slotted flaps

Structural hinge-moment increments caused by hinge-axis distortion

Two-dimensional wind-tunnel investigation of an approximately 14-percent-thick NACA 66-series-type airfoil section with a double slotted flap

Two-dimensional wind-tunnel investigation of sealed 0.22-airfoil-chord internally balanced ailerons of different contour on an NACA 65(112)- 213 airfoil

Resume of Wind-Tunnel Data on the Effect of External Stores on Stability of Models of Military Airplanes

An analysis of the indications of the University of Chicago airborne turbulence indicator in gusty air

A Preliminary Investigation of the Icing Characteristics of a Large Rectangular-Throat Pressure-Type Carburetor

An Experimental Investigation of Flow Conditions in the Vicinity of an NACA D(Sub S)-Type Cowling

Single-Cylinder Engine Tests of Porous Chrome-Plated Cylinder Barrels With Special Bore Coatings for Radial Air-Cooled Engines

Spray Characteristics of a Powered Dynamic Model of a Flying Boat Having a Hull With a Length-Beam Ratio of 9.0

Stalling of Helicopter Blades

A Preliminary Theoretical Study of Helicopter-Blade Flutter Involving Dependence Upon Coning Angle and Pitch Setting

Wind-Tunnel Investigation of an NACA 66-Series 16-Percent-Thick Low-Drag Tapered Wing With Fowler and Split Flaps

Tank Investigation of a Powered Dynamic Model of a Large Long-Range Flying Boat

Two-Dimensional Wind-Tunnel Investigation of Two NACA Low-Drag Airfoil Sections Equipped With Slotted Flaps and a Plain NACA Low-Drag Airfoil Section for XF6U-L Airplane

Static-Pressure Error of an Airspeed Installation on an Airplane in High-Speed Dives and Pullouts

Static-Thrust Investigation of Full-Scale PV-2 Helicopter Rotors Having NACA 0012.6 and 23012.6 Airfoil Sections

Strength Investigations in Aircraft Construction Under Repeated Application of the Load

Progress Report on Strength and Creep of Special Ceramic Bodies in Tension at Elevated Temperatures

Some Notes on the Effects of Jet-Exit Design on Static Longitudinal Stability

Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 6 Degrees and 9 Degrees Trim and a 22-1/2 Degree Angle of Dead Rise

Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 12 Degree Trim and With a 22-1/2 Degree Angle of Dead Rise

Wind-Tunnel Investigation of Control-Surface Characteristics of Plain and Balanced Flaps on an NACA 0009 Elliptical Semispan Wing

Wind-Tunnel Tests to Determine Aileron Characteristics of the McDonnell XFD-1 Airplane, TED No. NACA 23102

A Correlation of the Effects of Compression Ratio and Inlet-Air Temperature on the Knock Limits of Aviation Fuels in a CFR Engine 2

Kinetics of Chemical Reactions in Flames

Wind-Tunnel Tests and Analysis of Three 10-Foot-Diameter Three-Blade Tractor Propellers Differing in Pitch Distribution

Tests of the Jet-Motor Air-Intake Duct System on a 1/4-Scale Stub-Wing Model of a Pursuit-Type Airplane


Published Year

Subject

Author

‹‹ previous 1 2 ... 92 93 94 95 96 97 98 ... 280 281 next ››