Browse TRAIL Inventories

An Evaluation of a Rolleron-Roll-Rate-Stabilization System for a Canard Missile Configuration at Mach Numbers From 0.9 to 2.3

An Evaluation of the Roll-Rate Stabilization System of the Sidewinder Missile at Mach Numbers from 0.9 to 2.3

Ditching Investigation of a 1/11-Scale Model of the Chance Vought F7U-3 Airplane, TED NO. NACA DE 360

Ditching Investigation of a 1/20-Scale Model of the Boeing Stratocruiser Airplane (C-97)

Apparatus for Measurements of Time and Space Correlation

Low-Lift Drag of the Grumman F9F-9 Airplane as Obtained by a 1/7.5-Scale Rocket-Boosted Model and by Three 1/45.85-Scale Equivalent-Body Models Between Mach Numbers of 0.8 and 1.3, Ted No. NACA DE 391

Qualitative Results from a Flight Investigation to Determine Aileron Effectiveness of Two Rocket-Propelled 1/20-Scale Models of the MX-76 Missile

Chemical and Physical Properties of Hi-Cal-2

Component Performance Investigation of J71 Type II Turbines 5 - Internal Flow Conditions of J71 Type IIA Turbine

Component Performance Investigation of J71 Type II Turbines 3 - Overall Performance of J71 Type IIA Turbine

Altitude-Test-Chamber Investigation of the Endurance and Performance Characteristics of the J65-W-7 Engine at a Mach Number of 2.0

Aerodynamic Loads on an External Store Adjacent to a 45 Degree Sweptback Wing at Mach Numbers From 0.70 to 1.96, Including an Evaluation of Techniques Used

High-Speed Cascade Tests of the NACA 65-(12A(sub 10))10 and NACA 65-(12A(sub 2)I(sub 8b))10 Compressor Blade Sections

Injection Principles from Combustion Studies in a 200-Pound-Thrust Rocket Engine Using Liquid Oxygen and Heptane

NACA Conference on Aerodynamics of High-Speed Aircraft

An Investigation of the Maximum Lift of Wings at Supersonic Speeds

Investigation in the Langley Free-Flight Tunnel of the Low-Speed Stability and Control Characteristics of a 1/10-Scale Model Simulating the Convair F-102A Airplane

Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of the Sidewinder Missile at Mach Numbers from 1.2 to 2.1

Aerodynamic Design of Axial-flow Compressors 6 - Experimental Flow in Two-Dimensional Cascades

Supplementary Investigation in the Langley Free-Spinning Tunnel of a 1/20-Scale Model of the Douglas XF4D-1 Airplane Including Spin-Recovery Parachute Tests of the Model Loaded to Simulate the Douglas F5D-1 Airplane

Preliminary Results of the Determination of Inlet-Pressure Distortion Effects on Compressor Stall and Altitude Operating Limits of the J57-P-1 Turbojet Engine

Free-Spinning Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane, TED No. NACA AD 395

Free-Stream Boundaries of Turbulent Flows

Analysis and Calculation by Integral Methods of Laminar Compressible Boundary-Layer With Heat Transfer and With and Without Pressure Gradient

General theory of conical flows and its application to supersonic aerodynamics

Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4

Correlation of flight and analog investigations of roll coupling

Preliminary attempts at isothermal compression of a supersonic air stream

Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles

Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades

Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades

Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds

Effect of a reduction in stator solidity on performance of a transonic turbine

Visual study of free convection in a narrow vertical enclosure

Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant.

Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation

Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics

An analog study of a shock-position diffuser control on a supersonic turbojet engine

Some recent research on the handling qualities of airplanes

Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine

Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds

Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds

Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule

A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers

Flight and analytical study of roll requirements of a fighter airplane

Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds

Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8

The use of the horizontal tail for roll control

Factors affecting the maximum lift-drag ratio at high supersonic speeds

Spinning and related problems at high angles of attack for high-speed airplanes


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