TRAIL - Technical Report Archive and Image Library

Data presentation of force characteristics of several engine-strut-body configurations at Mach numbers of 1.8 and 2.0 / Robert T. Madden and Emil J. Kremzier

Effects of altitude on turbojet engine performance

Base pressures measured on several parabolic-arc bodies of revolution in free flight at Mach numbers from 0.8 to 1.4 and at large Reynolds numbers

Basic pressure measurements on a fuselage and a 45 degrees sweptback wing-fuselage combination at transonic speeds in the slotted test section of the Langley 8-foot high-speed tunnel

Aerodynamic characteristics of the NACA RM-10 research missile in the Ames 1- by 3-foot supersonic wind tunnel no. 2: Pressure and force measurements at Mach numbers of 1.52 and 1.98

Wind-tunnel tests of a 1/12-scale model of the X-3 airplane at subsonic and supersonic speeds.

Comparison of drag, pressure recovery, and surface pressure of a scoop-type inlet and an NACA submerged inlet at transonic speeds

A specially constructed metallograph for use at elevated temperatures

Relation of engine turbine-blade life to stress-rupture properties of the alloys, Stellite 21, Hastelloy B, Cast S-816, Forged S-816, X-40, Nimonic 80, Refractory 26, N-155, and Iconel X

A recurrence matrix solution for the dynamic response of aircraft in gusts

Investigation of the liquid fluorine-liquid diborane propellant combination in a 100-pound-thrust rocket engine

Buckling of thin-walled cylinder under axial compression and internal pressure

Variation of the pressure limits of flame propagation with tube diameter for propane-air mixtures

Vaporization rates and heat-transfer coefficients for pure liquid drops

Experimental investigation of typical constant- and variable-area exhaust nozzles and effects on axial-flow turbojet-engine performance

The effects at transonic speeds of thickening the trailing edge of a wing with a 4-percent-thick circular-arc airfoil

An investigation of the control-surface flutter derivatives of an NACA 65(sub 1)-213 airfoil in the Ames 16-foot high-speed wind tunnel

Direct-reading design charts for 75S-T6 aluminum-alloy flat compression panels having longitudinal extruded Z-section stiffeners

Experimental investigation of turbojet-engine thrust augmentation by combined compressor coolant injection and tail-pipe burning

The effects on the aerodynamic characteristics of reversing the wing of a triangular wing-body combination at transonic speeds as determined by the NACA wing-flow method

Comparison of airfoil sections on two triangular-wing-fuselage configurations at transonic speeds from tests by the NACA wing-flow method

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Body of revolution

A Simplified Instrument for Recording and Indicating Frequency and Intensity of Icing Conditions Encountered in Flight

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

A Summary of Meteorological Conditions Associated With Aircraft Icing and a Proposed Method of Selecting Design Criterions for Ice-Protection Equipment

Study of Chromium-Frit-Type Coatings for High-Temperature Protection of Molybdenum

Comparison of Heat Transfer from Airfoil in Natural and Simulated Icing Conditions

Investigation at Low Speed of 45 Degrees and 60 Degrees Sweptback, Tapered, Low-Drag Wings Equipped With Various Types of Full-Span, Trailing-Edge Flaps

Skin Friction of Incompressible Turbulent Boundary Layer Under Adverse Pressure Gradients

Transformations of the Hodograph Flow Equation and the Introduction of Two Generalized Potential Functions

Relative Structural Efficiencies of Flat Balsa-Core Sandwich and Stiffened-Panel Construction

Wing-Tunnel Investigation of Effects of Various Aerodynamic Balance Shapes and Sweepback on Control-Surface Characteristics of Semispan Tail Surfaces With NACA 0009, 0015, 66-009, 66(215)-014, and Circular-Arc Airfoil Sections

Width of Debye-Scherrer Lines for Finite Spectral Width of Primary Beam

Axial-Momentum Theory for Propellers in Compressible Flow

Calculation of Higher Approximations for Two-Dimensional Compressible Flow by a Simplified Iteration Process

A Survey of Creep in Metals

A Survey of Methods for Determining Stability Parameters of an Airplane From Dynamic Flight Measurements

The Linearized Characteristics Method and Its Application to Practical Nonlinear Supersonic Problems

Experimental Investigations of Rolling Performance of Straight and Sweptback Flexible Wings With Various Ailerons

A General Through-Flow Theory of Fluid Flow With Subsonic or Supersonic Velocity in Turbomachines of Arbitrary Hub and Casing Shapes

Rotogenerative Detection of Corrosion Currents

Construction and Use of Charts in Design Studies of Gas Turbines

A Theory of Conductivity of Cold-Worked Copper

Theoretical and Experimental Investigation of Condensation of Air in Hypersonic Wind Tunnels

Method for Analyzing Indeterminate Structures Stressed Above Proportional Limit

Numerical Determination of Indicial Lift of a Two-Dimensional Sinking Airfoil at Subsonic Mach Numbers From Oscillatory Lift Coefficients With Calculations for Mach Number 0.7

Approximate Calculation of Turbulent Boundary-Layer Development in Compressible Flow

Rectangular-Wind-Tunnel Blocking Corrections Using the Velocity-Ratio Method

Viscosities of Air and Nitrogen at Low Pressures

On the Application of Mathieu Functions in the Theory of Subsonic Compressible Flow Past Oscillating Airfoils

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