Browse TRAIL Inventories

On the Instability of Methods for the Integration of Ordinary Differential Equations

Tests to Determine the Adhesive Power of Passenger-Car Tires

Flow of Gas Through Turbine Lattices

Adaptation of Combustion Principles to Aircraft Propulsion Volume 2: Combustion in Air-Breathing Jet Engines

The Aerodynamic Characteristics in Pitch of a 1/15-Scale Model of the Grumman F11F-1 Airplane at Mach Numbers of 1.41, 1.61, and 2.01, TED No. NACA DE 390

Safeguards Against Flutter of Airplanes

Free-Spinning and Recovery Characteristics of a 1/19-Scale Model of the North American T-28C Airplane, TED No. NACA AD 3127

Effects of Intermittent Versus Continuous Heating upon the Tensile Properties of 2024-T4, 6061-T6 and 7075-T6 Alloys

Finite Span Wings in Compressible Flow

Flat Plate Cascades at Supersonic Speed

On the Contribution of Turbulent Boundary Layers to the Noise Inside a Fuselage

Fatigue-Crack Propagation in Aluminum Alloy Box Beams

Supersonic flow past nonlifting bumped and indented bodies of revolution

Static lateral stability and control characteristics of a model of a 45 degree swept-wing fighter airplane with various vertical tails at Mach numbers of 1.41, 1.61, and 2.01

Aircraft configurations developing high lift-drag ratios at high supersonic speeds

Performance of Inconel 739 Buckets in J33-9 Turbojet Engine

Experimental Results From a Test in Rough Air at High Subsonic Speeds of a Tailless Rocket Model Having Cruciform Triangular Wings, and a Note on the Calculation of Mean Square Loads of Aircraft in Continuous Rough Air

Experimental Transonic Flutter Characteristics of an Untapered, 45 Degree Sweptback, Aspect Ratio 4 Wing

An Experimental Investigation of the Effects of Several Diffusers and Diffuser-Entrance-Mixing-Section Combinations on the Power Requirements of a 4 1/2-Inch by 4 1/2-Inch Slotted Transonic Wind Tunnel

Exploratory Investigation of the Use of Area Suction to Eliminate Air-Flow Separation in Diffusers Having Large Expansion Angles

External-Store Drag Reduction at Transonic and Low Supersonic Mach Numbers by Application of Baldwin's Moment-of-Area Rule

Exploratory Materials and Missile-Nose-Shape Tests in a 4,000 Degrees F Supersonic Air Jet

Exploratory Investigation of a Helicopter Pressure-Jet System on the Langley Helicopter Test Tower

Experimental Measurements of Forces and Moments on a Two-Dimensional Oscillating Wing at Subsonic Speeds

Experimental Investigation of Turbine Stator-Blade-Outlet Boundary-Layer Characteristics and a Comparison With Theoretical Results

Experimental Steady-State Yawing Derivatives of a 60 Degree Delta-Wing Model as Affected by Changes in Vertical Position of the Wing and in Ratio of Fuselage Diameter to Wing Span

Experimental Investigation of Marquardt Shock-Positioning Control Unit on a 28-Inch Ram-Jet Engine

Some Effects of Roll Rate on the Longitudinal Stability Characteristics of a Cruciform Missile Configuration as Determined From Flight Test for a Mach Number Range of 1.1. To 1.8

Some Effects of Wing Fences on the Lateral Stability Derivatives of a 60 Degree Delta Wing Oscillating Continuously in Yaw

Some Measurements of Aerodynamic Forces and Moments at Subsonic Speeds on a Wing-Tank Configuration Oscillating in Pitch About the Wing Midchord

Some Wind-Tunnel Experiments on Single-Degree-of-Freedom Flutter of Ailerons in the High Subsonic Speed Range

Preliminary Report on Experimental Investigation of Engine Dynamics and Controls for a 48-Inch Ram-Jet Engine

Preliminary Measurements of the Aerodynamic Yawing Derivatives of a Triangular, a Swept, and an Unswept Wing Performing Pure Yawing Oscillations, With a Description of the Instrumentation Employed

Tabulation of Mass-Flow Parameters for Use in Design of Turbomachine Blade Rows for Ratios of Specific Heats of 1.3 and 1.4

Comparison of the Minimum Drag of Two Versions of a Modified Delta-Wing Fighter as Obtained From Flight Tests of Rocket-Boosted Models and Equivalent Bodies Between Mach Numbers of 0.80 and 1.64

Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels

Turbulent and Laminar Heat-Transfer Measurements on a 1/6-Scale NACA RM-10 Missile in Free Fight to Mach Number of 4.2 and to a Wall Temperature of 1400 Degrees R

Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane

Turbulent-Heat-Transfer Measurements at a Mach Number of 3.90

The Use of Area Suction for Improving the Longitudinal Characteristics of a Thin Unswept Wing-Fuselage Model With Leading- and Trailing-Edge Flaps

Two Experiments on Applications of the Transonic Area Rule to Asymmetric Configurations

Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-Sided Fuselage: Lift, Drag, Longitudinal Stability, Lateral Force, and Jet Effects at Mach Numbers Between 1.0 and 2.3

Static Shear Strength of 2117-T4 (A17S-T4) Aluminum-Alloy Rivets at Elevated Temperatures

The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin

Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration

A Semiempirical Procedure for Estimating Wing Buffet Loads in the Transonic Region

A Semigraphical Method for the Determination of the Rolling Characteristics of Rolleron-Equipped Missiles

Pressure Distributions on Four Canopy-Fuselage Configurations at Transonic Speeds

Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6

Some Effects of Sweep and Thickness on the Experimental Downwash Characteristics at Transonic Speeds of a Series of Highly Tapered Wings With an Aspect Ratio of 3: Transonic Bump Method


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