Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
4176 results returnedSearch results
- Intercooler cooling-air weight flow and pressure drop for minimum drag loss
- An investigation of aircraft heaters 15: the emissivity of several materials
- An investigation of aircraft heaters 14: an air and heat flow analysis of a ram-operated heater and duct system
- An investigation of aircraft heaters 24: the heat meter in the transient state for unidirectional heat transfer
- An interim report on the stability and control of tailless airplanes
- A method for welding sheet aluminum to SAE 4140 steel
- A method for the rapid estimation of turbulent boundary-layer thickness for calculating profile drag
- Loss of xylidines in overwater storage of xylidine-blended fuel
- Performance tests of NACA type A finned-tube exhaust heat exchanger
- Oxygen boosting of an aircraft-engine cylinder in conjunction with internal coolants
- A preliminary evaluation of the explosion jet-propulsion engine
- Longitudinal characteristics and aileron effectiveness of a midwing airplane from high-speed wind tunnel tests
- Measurement of free water in cloud under conditions of icing
- Flame-visibility tests with individual exhaust stacks
- Flight tests of the thermal ice-prevention equipment on the B-17F airplane
- Flight tests of various tail modifications on the Brewster XSBA-1 airplane III : measurements of flying qualities with tail configuration 3
- Flight tests of several exhaust-gas-to-air heat exchangers
- Flight tests of a pursuit airplane fitted with an experimental bellows-type bob weight
- Gasoline-water distribution coefficients of 27 aromatic amines
- Note on the interpretation of wake-survey data and its use in the estimation of induced drag due to irregularities
- Wind-Tunnel Procedure for Determination of Critical Stability and Control Characteristics of Airplanes
- The effect of compression ratio, cooled exhaust gas mixed with inlet air, and inlet-air temperature on the knock-limited performance of a full-scale single-cylinder engine
- The effect of continuous knock on the endurance of an aircraft engine cylinder
- Effect of coaxial lapping of cast-iron piston rings on ring performance
- Knock-limited performance of several internal coolants
- Knock-limited performance of several internal coolants
- Ditching tests with a 1/12-size model of the Army B-26 airplane in NACA tank number 2 and on an outdoor catapult
- Determination of jet-boundary corrections to cowling-flap-outlet pressures by an electrical analogy method
- The design of the optimum hull for a large long-range flying boat
- Preignition-limited performance of several fuels
- Knock-limited power outputs from a CFR engine using internal coolants 1: monomethylamine and dimethylamine
- Effect of Mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing
- Airfoil section data from tests of 10 practical- construction sections of helicopter rotor blades submitted by the Sikorsky Aircraft Division, United Aircraft Corporation
- Airfoil-contour modifications based on (epsilon)-curve method of calculating pressure distribution
- Cascade investigation of buckets for a modern aircraft turbosupercharger
- An analytical investigation of thermal-electric means of preventing ice formations on a propeller blade
- Bending and shear stresses developed by the instantaneous arrest of the root of a moving cantilever beam
- Compressibility and heating effects on pressure loss and cooling of a baffled cylinder barrel
- Compressible potential flow with circulation about a circular cylinder
- Analysis of factors affecting net lift increment attainable with trailing-edge split flaps on tailless airplanes
- Analysis of a thermal ice-prevention system for wing leading-edge landing-light installations
- Analysis of available data on the effectiveness of ailerons without exposed overhang balance
- Effect of water injection on knock-limited performance of a V-type 12-cylinder liquid-cooled engine
- Effect of tilt of the propeller axis on the longitudinal-stability characteristics of single-engine airplanes
- Determination of the effect of wing flexibility on lateral maneuverability and a comparison of calculated rolling effectiveness with flight results
- The determination of span load distribution at high speeds by use of high-speed wind-tunnel section data
- Effect of tilt of the propeller axis on the longitudinal-stability characteristics of single-engine airplanes
- Estimation of pressures on cockpit canopies, gun turrets, blisters, and similar protuberances
- Estimation of pressure distributions at subcritical speeds for turrets located on a wing
- Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails