TRAIL - Technical Report Archive and Image Library

Flight measurements of drag and base pressure of a fin-stabilized parabolic body of revolution (NACA RM-10) at different Reynolds numbers and at Mach numbers from 0.9 to 3.3

Determination of flame temperatures from 2000 to 3000 K by microwave absorption

Design considerations for wings having minimum drag due to lift

Design data for multipost-stiffened wings in bending

An analytical estimation of the effect of transpiration cooling on the heat-transfer and skin-friction characteristics of a compressible, turbulent boundary layer

An analytical investigation of airplane spin-recovery motion by use of rotary-balance aerodynamic data

Comparison of model and full-scale spin recoveries obtained by use of rockets

Comparison of flutter calculations using various aerodynamic coefficients with experimental results for some rectangular cantilever wings at Mach number 1.3

Combined natural- and forced-convection laminar flow and heat transfer of fluids with and without heat sources in channels with linearly varying wall temperatures

Effect of various arrangements of triangular ledges on the performance of a 23 degree conical diffuser at subsonic Mach numbers

Evaluation of the accuracy of an aircraft radio altimeter for use in a method of airspeed calibration

Examination of the existing data on the heat transfer of turbulent boundary layers at supersonic speeds from the point of view of Reynolds analogy

An evaluation of the soap-bubble method for burning velocity measurements using ethylene-oxygen-nitrogen and methane-oxygen-nitrogen mixtures

Tables for the computation of wave drag of arrow wings of arbitrary airfoil section

An evaluation of an accelerometer method for obtaining landing-gear drag loads

Minimum-wave-drag airfoil section for arrow wings

Effects of leading-edge radius and maximum thickness-chord ratio on the variation with Mach number of the aerodynamic characteristics of several thin NACA airfoil sections

The effectiveness at high subsonic Mach numbers of a 20-percent-chord plain trailing-edge flap on the NACA 65-210 airfoil section

An experimental and theoretical investigation of the anisotropy of 3S aluminum-alloy sheet in the plastic range

Experimental determination of boundary-layer transition on a body of revolution at M = 3.5

Experimental investigation of heat-transfer and fluid-friction characteristics of white fuming nitric acid

Experimental investigation of temperature recovery factors on a 10 degree cone at angle of attack at a Mach number of 3.12

Impingement of Water Droplets on an Ellipsoid with Fineness Ration 10 in Axisymmetric Flow

A simple mechanical analogue for studying the dynamic stability of aircraft having nonlinear moment characteristics

Shock-turbulence interaction and the generation of noise

Shocks in helical flows through annular cascades of stator blades

Some new drag data on the NACA RM-10 missile and a correlation of the existing drag measurements at M = 1.6 and 3.0

Some measurements and power spectra of runway roughness

Some measurements of atmosphere turbulence obtained from flow-direction vanes mounted on an airplane

A simplified mathematical model for calculating aerodynamic loading and downwash for wing-fuselage combinations with wings of arbitrary plan form

Static properties and resistance characteristics of a family of seaplane hulls having varying length-beam ratio

Relation of microstructure to high-temperature properties of a wrought cobalt-base alloy stellite 21 (AMS 5385)

The resistance to air flow of porous materials suitable for boundary-layer-control applications using area suction

Section characteristics of an NACA 0006 airfoil with area suction near the leading edge

Organophosphorus Compounds in Rocket-Engine Applications

Preliminary Flight Measurements of the Total-Pressure Recovery of a Split-Wing Ram-Jet Inlet at Mach Numbers from 1.4 to 3.16

Experimental Investigation of Sublimation of Ice at Subsonic and Supersonic Speeds and Its Relation to Heat Transfer

Speed-Brake Investigation at Low Speed of a 1/10-Scale Model of the MX-1554A Airplane With a Circular Jet Nozzle

Preliminary Performance Data Obtained in a Full-Scale Free-Jet Investigation of a Side-Inlet Supersonic Diffuser

On the Three-Dimensional Instability of Laminar Boundary Layers on Concave Walls

A Transonic Wind-Tunnel Investigation of the Performance and of the Static Stability and Control Characteristics of a 1/15-Scale Model of the Grumman F9F-9 Airplane, Ted No. NACA DE 390

Summary of the Lift, Drag, and Stability of 1/10-Scale Rocket-Boosted Models of the McDonnell XF3H-1 Airplane for a Mach Number Range of 0.6 to 1.4 as Affected by the Operation of Extensible Rocket Racks

Rocket-Model Investigation of the Longitudinal Stability, Drag, and Duct Performance of a 60 Degree Delta-Wing Canard Aircraft With Twin Side Inlets at Mach Numbers From 0.80 to 1.70

Rocket-Powered-Model Investigation of the Effects of Aeroelasticity on the Rolling Effectiveness of an 8.06-Percent-Scale McDonnell F3H-1 Airplane Wing at Mach Numbers From 0.5 to 1.4

Preliminary Transient Performance Data on the Fuel Control of the XRJ47-W-5 Ram-Jet Engine

A Procedure for the Design of Air-Heated Ice-Prevention Systems

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