Browse TRAIL Inventories

Effect of Fuel Volatility on Performance of Tail-Pipe Burner

Supersonic Tunnel Investigation by Means of Inclined-Plate Technique to Determine Performance of Several Nose Inlets Over Mach Number Range of 1.72 to 2.18

Studies of Von Kármán's Similarity Theory and Its Extension to Compressible Flows: A Similarity Theory for Turbulent Boundary Layer Over a Flat Plate in Compressible Flow

Studies of Von Kármán's Similarity Theory and Its Extension to Compressible Flow: Investigation of Turbulent Boundary Layer Over a Flat Plate in Compressible Flow by the Similarity Theory

Survey of Available Information on Internal Flow Losses Through Axial Turbomachines

Secondary Stresses in Thin-Walled Beams With Closed Cross Sections

Methods for Connection to Revolving Thermocouples

Performance of a Cascade in an Annular Vortex-Generating Tunnel Over Range of Reynolds Numbers

Application of Variational Methods to Transonic Flows With Shock Waves

Investigations of Slot Configurations for Film-Cooled Turbine Blades by Flow Visualization Methods

Deflections of a Simply Supported Rectangular Sandwich Plate Subjected to Transverse Loads

Limits of Flammability of Pure Hydrocarbon-Air Mixtures at Reduced Pressures and Room Temperature

Investigation of the Structural Damping of a Full-Scale Airplane Wing

Effects of Wing Position and Horizontal-Tail Position on the Static Stability Characteristics of Models With Unswept and 45 Degree Sweptback Surfaces With Some Reference to Mutual Interference

Effect of Angle of Attack and Exit Nozzle Design on the Performance of a 16-Inch Ram Jet at Mach Numbers From 1.5 to 2.0

Hydrodynamic Investigation of a Series of Hull Models Suitable for Small Flying Boats and Amphibians

Generalized Linearized Conical Flow

Flight Investigation of the Effect of Atmospheric Turbulence on the Climb Performance of an Airplane

A Flight Investigation of the Effect of Center-of-Gravity Location on Gust Loads

Study of Vortex Shedding as Related to Self-Excited Torsional Oscillations of an Airfoil

Theoretical and Experimental Investigation of Additive Drag

Some Effects of Blade Trailing-Edge Thickness on Performance of a Single-Stage Axial-Flow Compressor

Review of Problems of Conservation of Strategic Materials for Turbine Engines

Observations on Bauschinger Effect in Copper and Brass

Tensile Fracturing Characteristics of Several High-Temperature Alloys as Influenced by Orientation in Respect to Forging Direction

On the Attached Curved Shock in Front of a Sharp-Nosed Axially Symmetrical Body Placed in a Uniform Stream

Review of Current and Anticipated Lubricant Problems in Turbojet Engines

An Electromagnetic Flowmeter for Rocket Research

Internal Flow and Burning Characteristics of 16-inch Ram Jet Operating in a Free Jet at Mach Numbers of 1.35 and 1.73

Notes on Heat-Resistant Materials in Britain from Technical Mission October 13 to November 30, 1950

A Semiempirical Procedure for Computing the Water-Pressure Distribution on Flat and V-Bottom Prismatic Surfaces During Impact or Planing

Measurements in Flight of the Longitudinal Characteristics of Two Jet Aircraft, One With a Diving Tendency and the Other With a Climbing Tendency at High Mach Numbers

Influence of Wing and Fuselage on the Vertical-Tail Contribution to the Low-Speed Rolling Derivatives of Midwing Airplane Models with 45 Degree Sweptback Surfaces

Experimental Investigation of the Low-Speed Static and Yawing Stability Characteristics of a 45 Degrees Sweptback High-Wing Configuration with Various Twin Vertical Wing Fins

Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0

Effects of Several Arrangements of Rectangular Vortex Generators on the Static-Pressure Rise Through a Short 2:1 Diffuser

Effects of Design Details on the Fatigue Strength of 355-T6 Sand-Cast Aluminum Alloy

Evaluation of High-Angle Attack Aerodynamic-Derivative Data and Stall-Flutter Prediction Techniques

Experimental Pressure Distributions Over Two Wing-Body Combinations at Mach Number 1.9

Power Unit for High-Intensity Light Source

Mechanical and Corrosion Tests of Spot-Welded Aluminum Alloys

Lift, Drag, and Pitching Moment of Low-Aspect-Ratio Wings at Subsonic and Supersonic Speeds : Plane Tapered Wing of Aspect Ratio 3.1 with 3-Percent-Thick, Biconvex Section

Preliminary Investigation of the Control of a Gas-Turbine Engine for a Helicopter

The Forces and Pressure Distribution at Subsonic Speeds on a Plane Wing Having 45 Degrees of Sweepback, an Aspect Ratio of 3, and a Taper Ratio of 0.5

Calculated Performance of a Direct-Air Nuclear Turbojet-Powered Airplane Using a Split-Flow Reactor and a Separated-Type Shield

Combustion-Chamber Performance Characteristics of a Python Turbine-Propeller Engine Investigated in Altitude Wind Tunnel

Sideslip in a Viscous Compressible Gas

Lateral Control by Spoilers at the DVL

On the Problem of Gas Flow Over an Infinite Cascade Using Chaplygin's Approximation

On the Theory of Thin and Thin-Walled Rods


Published Year

Subject

Author

‹‹ previous 1 2 ... 21 22 23 24 25 26 27 ... 143 144 next ››