Browse TRAIL Inventories

Investigation of Spoilers at a Mach Number of 1.93 to Determine the Effects of Height and Chordwise Location on the Section Aerodynamic Characteristics of a Two-Dimensional Wing

Investigation of Tantalum in a 3,800 Degrees Fahrenheit Supersonic Airstream

Investigation of Flutter Characteristics of Three Low-Aspect-Ratio All-Movable Half-Span Control Surfaces at Mach Numbers From 1.49 to 2.87

Investigation of the Longitudinal Aerodynamic Characteristics of a Trapezoidal-Wing Airplane Model With Various Vertical Positions of Wing and Horizontal Tail at Mach Numbers of 1.41 and 2.01

Analysis of Turbulent Flow and Heat Transfer in Noncircular Passages

Experimental Investigation of the Lateral Trim of a Wing-Propeller Combination at Angles of Attack Up to 90 Degrees With All Propellers Turning in the Same Direction

Theoretical Calculations of Supersonic Wave Drag at Zero Lift for a Particular Store Arrangement

Theoretical Rocket Performance of JP-4 Fuel with Several Fluorine-Oxygen Mixtures Assuming Equilibrium Composition

Theoretical Rocket Performance of Liquid Methane with Several Fluorine-Oxygen Mixtures Assuming Frozen Composition

Hydrodynamic Characteristics of a Model of a Proposed Six-Engine Hull-Type Seaplane Designed for Supersonic Flight

Flight Tests of Two Smoke-Producing Devices Having Deacon Rocket Boosters

Heat Transfer for Mach Numbers Up to 2.2 and Pressure Distributions for Mach Numbers Up to 4.7 From Flight Investigations of a Flat-Face-Cone and a Hemisphere-Cone

Heat Transfer Measured on a Flat-Face Cylinder-Flare Configuration in Free Flight at Mach Numbers From 1.6 to 2.7

Further Investigation of Fatigue-Crack Propagation in Aluminum-Alloy Box Beams

Heat-Transfer and Pressure Measurements From a Flight Test of the Second 1/18-Scale Model on the Titan Intercontinental Ballistic Missile Up to a Mach Number of 3.91 and Reynolds Number Per Foot of 23.4 X 10(Exp 6) : Coord. No. AF-AM-70

Investigation of a Tilting-Wing Vertical-Take-Off-and-Landing Jet Airplane Model in Hovering and Transition Flight

Investigation of a High-Flow Transonic-Compressor Inlet Stage Having a Hub-Tip Radius of 0.35

Fatigue Behavior of Aircraft Structural Beams

Relationship of Metal Surfaces to Heat-Aging Properties of Adhesive Bonds

A Low-Speed Experimental Investigation of the Effect of a Sandpaper Type of Roughness on Boundary-Layer Transition

Aerodynamic Effects Caused by Icing of an Unswept NACA 65A004 Airfoil

Acoustic, thrust, and drag characteristics of several full-scale noise suppressors for turbojet engines

Accelerations in Transport-Airplane Crashes

Studies of OH, CO, CH, and C₂ Radiation From Laminar and Turbulent Propane-Air and Ethylene-Air Flames

Longitudinal and Lateral Stability and Control Characteristics at Mach Number 2.01 of a 60 Degree Delta-Wing Airplane Configuration Equipped With a Canard Control and With Wing Trailing-Edge Flap Controls

Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04

Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3

Experimental techniques for predicting store motions during release or ejection

Recent control studies

Some Research on the Lift and Stability of Wing-Body Combinations

An analytical evaluation of the effects of an aerodynamic modification and of stability augmenters on the pitch behavior and probable pilot opinion of two current fighter airplanes

Effects of Components and Various Modifications on the Drag and the Static Stability and Control Characteristics of a 42 Deg Swept-Wing Fighter-Airplane Model at Mach Numbers of 1.60 to 2.50

Boundary-Layer Displacement Effects in Air at Mach Numbers of 6.8 and 9.6

Forty-Fourth Annual Report of the National Advisory Committee for Aeronautics Administrative Report Including Technical Reports Nos. 1342 to 1392

Spin-Tunnel Investigation of a 1/28-Scale Model of a Subsonic Attack Airplane

Spin Tunnel Investigation of a 1/30 Scale Model of the North American A-5A Airplane

Flow and Drag Formulas for Simple Quadrics

Graphic Construction of Joukowski Wings

The Aerodynamic Forces on Airship Hulls

Applications of Modern Hydrodynamics to Aeronautics Part 1: Fundamental Concepts and the Most Important Theorems. Part 2: Applications

The Minimum Induced Drag of Aerofoils

Flow and Force Equations for a Body Revolving in a Fluid

Determination of the local heat-transfer characteristics on glaze ice accretions on a cylinder and a NACA 0012 airfoil

The Theory of the Pitot and Venturi Tubes, Part 2

Unsteady flow past a NACA 0012 airfoil pitching at constant rates


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