Browse TRAIL Inventories

Analysis of the High-Altitude Cooling of the Ranger SGV-770 D-4 Engine in the Bell XP-77 Airplane

Effect of Turbulence on Air-Flow Measurements Behind Orifice Plates

High-Altitude Cooling 3: Radiators

Compressibility Effects on Heat Transfer and Pressure Drop in Smooth Cylindrical Tubes

Investigation of wing characteristics at a Mach number of 1.53 1: triangular wings of aspect ratio 2

Effect of Aspect Ratio and Taper on the Pressure Drag at Supersonic Speeds of Unswept Wings at Zero Lift

Investigation of wing characteristics at a Mach number of 1.53 3: unswept wings of differing aspect ratio and taper ratio

Charts for the conical part of the downwash field of swept wings at supersonic speeds

Calculative method for estimating the interference pressure field at zero lift on a symmetrical swept-back wing mounted on a circular cylindrical body

Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02

Method for estimating lift interference of wing-body combinations at supersonic speeds

Method for Estimating Lift Interference of Wing-Body Combinations at Supersonic Speeds

Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds: Lift, pitching moment, and hinge moment

Wing-body interference at supersonic speeds with an application to combinations with rectangular wings

Lift and center of pressure of wing-body-tail combinations at subsonic, transonic, and supersonic speeds

Comparison between theory and experiment for interference pressure field between wing and body at supersonic speeds

Quasi-Cylindrical Theory of Wing-Body Interference at Supersonic Speeds and Comparison with Experiment

General theory of wave-drag reduction for combinations employing quasi-cylindrical bodies with an application to swept-wing and body combinations

Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02

Tables of Characteristic Functions for Solving Boundary-Value Problems of the Wave Equation with Application to Supersonic Interference

The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes

The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes


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