Browse TRAIL Inventories

Buffet Tests of an Attack-Airplane Model With Emphasis on Analysis of Data From Wind-Tunnel Tests

Aerodynamic Characteristics at a Mach Number of 6.8 of Two Hypersonic Missile Configurations, One With Low-Aspect-Ratio Cruciform Fins and Trailing-Edge Flaps and One With a Flared Afterbody and All-Movable Controls

Aerodynamic Load Distribution on a 45 Degree Sweptback Wing With Leading-Edge Chord-Extensions at Transonic Speeds, Including Effects of a Spoiler-Slot-Deflector Aileron

Aerodynamic Characteristics at Mach Numbers From 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight

Aerodynamic Performance and Static Stability and Control of Flat-Top Hypersonic Gliders at Mach Numbers From 0.6 to 18

Analytical and Experimental Investigation of Aerodynamic Forces and Moments on Low-Aspect-Ratio Wings Undergoing Flapping Oscillations

Longitudinal Stability Investigation of a Vertical-Take-Off-and-Landing Airplane Configuration With Simulated Jet Intake and Exhaust at Mach Numbers of 1.61 and 2.01

Low-Speed Boundary-Layer-Control Investigation on a Thin Rectangular Semispan Wing With Leading-Edge and Trailing-Edge Flaps

Measurements of Aerodynamic Heat Transfer on a 15 Degree Cone-Cylinder-Flare Configuration in Free Flight at Mach Numbers Up to 4.7

Investigation of Lithium Hydride and Magnesium as High-Temperature Internal Coolants With Several Skin Materials

An Investigation of the Effects of Atmospheric Corrosion on the Fatigue Life of Aluminum Alloys

An Investigation of the Effect of Target Temperature on Projectile Penetration and Cratering

Free Convection Under the Conditions of the Internal Problem

A Correlation of Results of Flight Investigation With Results of an Analytical Study of Effects of Wing Flexibility on Wing Strains Due to Gusts

Effect of Target-Type Thrust Reverser on Transonic Aerodynamic Characteristics of a Single-Engine Fighter Model

Effects of Boattail Area Contouring and Simulated Turbojet Exhaust on the Loading and Fuselage-Tail Component Drag of a Twin-Engine Fighter-Type Airplane Model

Aerodynamic Research on Fuselages with Rectangular Cross Section

Measurements of the Buffeting Loads on the Wing and Horizontal Tail of a 1/4-Scale Model of the X-1E Airplane

NACA Conference on High-Speed Aerodynamics

Longitudinal and Lateral Stability and Control Characteristics and Vertical-Tail-Load Measurements for a 0.03-Scale Model of the Avro CF-105 Airplane at Mach Numbers of 1.60, 1.80, and 2.00

NACA Research on Slurry Fuels

An Investigation of the Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane With Alternate Nose Configurations With and Without Wing Fuel Tanks, TED No. NACA AD 395

Stability of Cylindrical and Conical Shells of Circular Cross Section, with Simultaneous Action of Axial Compression and External Normal Pressure

The Turbulent Boundary Layer on a Rough Curvilinear Surface

Statistical Study of Turbulence: Spectral Functions and Correlation Coefficients

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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