Browse TRAIL Inventories

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


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