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


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