Browse TRAIL Inventories

Some Yawing Tests of a 1/30-Scale Model of the Hull of the XPB2M-1 Flying Boat

Theoretical Analysis of the Lateral Stability of a Glider Towed by Twin Parallel Towlines

Use of Stagnation Temperature in Calculating Rate of Heat Transfer in Aircraft Heat Exchangers

Wind-Tunnel Investigation of a Plain Aileron with Various Trailing-Edge Modifications on a Tapered Wing 3: Ailerons with Simple and Spring-Linked Balancing Tabs

Wind-Tunnel Investigation of an NACA 23012 Airfoil With a 0.30-Airfoil-Chord Double Slotted Flap

Wind-Tunnel Investigation of Control-Surface Characteristics 14: NACA 0009 Airfoil With a 20-Percent-Chord Double Plain Flap

Vibration Surveys of the P-47-B Rudder and Fin-Rudder Assembly

Vibration Surveys of the P-40 Rudder and Fin-Rudder Assembly

Wind-Tunnel Investigation of a Full-Span Retractable Flap in Combination With Full-Span Plain and Internally Balanced Ailerons on a Tapered Wing

The Measurement of Fuel-Air Ratio by Analysis of the Oxidized Exhaust Gas

The Advantages of Uniform Fuel Distribution for Air-Cooled Engines From Considerations of Cooling Requirements and Fuel Economy

Altitude Rating of Electrical Apparatus

Flight Investigation of NACA D(Sub S) Cowlings on the XP-42 Airplane 1: High-Inlet-Velocity Cowling with Propeller Cuffs Tested in High-Speed Level Flight

Antiknock Effectiveness of Xylidines in Small-Scale Engines

Wind Tunnel Tests of Ailerons at Various Speeds 5: Pressure Distributions Over the NACA 66,2-216 and NACA 23012 Airfoils With Various Balances on 0.20-Chord Ailerons

Wind-Tunnel Tests of a Piston-Type Control Booster on an Airfoil and Aileron Model

Wind Tunnel Tests of Ailerons at Various Speeds 1: Ailerons of 0.20 Airfoil Chord and True Contour With 0.35 Aileron-Chord Extreme Blunt Nose Balance on the NACA 66,2-216 Airfoil

Wind-Tunnel Investigation of Devices for Improving the Diving Characteristics of Airplanes

Wind-Tunnel Investigation of Rear Underslung Fuselage Ducts

Wind-Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics 5: Symmetrically Tapered Wing With a Circular Fuselage Having a Horizontal and a Vertical Tail

Tests of 10-Inch 24S-T Aluminum-Alloy Shear Panels With 1-1/2-Inch Holes

Tests of Inverted Spins in the NACA Free-Spinning Tunnels

Theory of Self-Excited Mechanical Oscillations of Hinged Rotor Blades

Theory of Mechanical Oscillations of Rotors With Two Hinged Blades

Tests of Exhaust Propulsion Nozzles

Tail Buffeting

Operating Temperatures of a Sodium-Cooled Exhaust Valve as Measured by a Thermocouple

Heat Transfer of Airfoils and Plates

Heat Transfer Over the Circumference of a Heated Cylinder in Transverse Flow

Experimental Investigation of a Model of a Two-Stage Turboblower

Experimental Investigation of Impact in Landing on Water

A Subpress for Compressive Tests

A Theoretical Investigation of the Lateral Oscillations of an Airplane With Free Rudder With Special Reference to the Effect of Friction

Notes on the Effect of Surface Distortions on the Drag and Critical Mach Number of Airfoils

Review of Flight Tests of NACA C and D Cowlings on the XP-42 Airplane

A Method of Estimating the Knock Rating of Hydrocarbon Fuel Blend

Protection of Nonmetallic Aircraft From Lighting 1: General Analysis

Protection of Nonmetallic Aircraft From Lightning 2: Lightning Conductor Materials

The Flow of a Compressible Fluid Past a Curved Surface

Working Charts for the Computation of Propeller Thrust Throughout the Take-Off Range

Tests of a 1/40-Scale Wing-Hull Model and a 1/10-Scale Float-Strut Model of the Hughes-Kaiser Cargo Airplane in the Two-Dimensional Low-Turbulence Pressure Tunnel

Tests of Airfoils Designed to Delay the Compressibility Burble

Tests in the NACA Two-Dimensional Low-Turbulence Tunnel of Airfoil Sections Designed to Have Small Pitching Moments and High Lift-Drag Ratios

Porpoising: A Comparison of Theory With Experiment

Wind-Tunnel Investigation of Wing Ducts on a Single Engine Pursuit Airplane

Methods and Charts for Computing Stability Derivatives of a V-Bottom Planing Surface

Effect of Length-Beam Ration on Resistance and Spray of Three Models of Flying-Boat Hulls

Investigation for the Development of a High-Speed Antiaircraft Tow Target

Free-Flight-Tunnel Investigation of the Effect of Mode of Propeller Rotation Upon the Lateral-Stability Characteristics of a Twin-Engine Airplane Model With Single Vertical Tails of Different Size

Flying Qualities and Stalling Characteristics of North American XP-51 Airplane


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