Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
14045 results returnedSearch results
- Initial results of instrument-flying trials conducted in a single-rotor helicopter
- Method for calculating the rolling and yawing moments due to rolling for unswept wings with or without flaps or ailerons by use of nonlinear section lift data
- The Langley annular transonic tunnel
- Time-History Data of Maneuvers Performed by a Republic F84G Airplane During Squadron Operational Training
- Design of two-dimensional channels with prescribed velocity distributions along the channel walls
- Analytical study of blockage- and lift-interference corrections for slotted tunnels obtained by the substitution of an equivalent homogeneous boundary for the discrete slots
- Air-water analogy and the study of hydraulic models
- Aerodynamic characteristics of low-aspect-ratio wings at high supersonic Mach numbers
- Aerodynamic characteristics of a refined deep-step planing-tail flying-boat hull with various forebody and afterbody shapes
- Aerodynamic forces and loadings on symmetrical circular-arc airfoils with plain leading-edge and plain trailing-edge flaps
- An analysis of laminar free-convection flow and heat transfer about a flat plate paralled to the direction of the generating body force
- A Brief Investigation of the Hydrodynamic Characteristics of a 1/13.33-Scale Powered Dynamic Model of a Preliminary Design of the Martin XP6M-1 Flying Boat, TED No. NACA DE-385
- Investigation of the Low-Speed Stability and Control Characteristics of a 1/10-Scale Model of the Convair YF-102 Airplane in the Langley Free-Flight Tunnel
- Wind-Tunnel Investigation of the Static Lateral Stability Characteristics of Wing-Fuselage Combinations at High Subsonic Speeds
- Wind-Tunnel Investigation at Low Speed of the Pitching Stability Derivatives of a 1/9-Scale Powered Model of the Convair XFY-1 Vertically Rising Airplane, TED No. NACA DE 373
- Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/9-Scale Powered Model of the Convair XFY-1 Vertically Rising Airplane, TED No. NACA DE 373
- Relative importance of various sources of defect-producing hydrogen introduced into steel during application of vitreous coatings
- Secondary flows and boundary-layer accumulations in turbine nozzles
- Survey of portions of the chromium-cobalt-nickel-molybdenum quaternary system at 1,200 degrees c
- Lateral Oscillatory Characteristics of the Republic F-91 Airplane Calculated by Using Low-Speed Experimental Static and Rotary Derivatives
- A Study of the Motion and Aerodynamic Heating of Missiles Entering the Earth's Atmosphere at High Supersonic Speeds
- Dynamics of mechanical feedback-type hydraulic servomotors under inertia loads
- Prediction of flame velocities of hydrocarbon flames
- Charts and approximate formulas for the estimation of aeroelastic effects of the lateral control of swept and unswept wings
- Charts and approximate formulas for the estimation of aeroelastic effects on the loading of swept and unswept wings
- Considerations on the effect of wind-tunnel walls on oscillating air forces for two-dimensional subsonic compressible flow
- Comparison of effectiveness of convection-, transpiration-, and film-cooling methods with air as coolant
- Study of inadvertent speed increases in transport operation
- Application of a channel design method to high-solidity cascades and tests of an impulse cascade with 90 degrees of turning
- Preliminary Appraisal of Ferrocene as an Igniting Agent for JP-4 Fuel and Fuming Nitric Acid
- A comparison of the experimental subsonic pressure distributions about several bodies of revolution with pressure distributions computed by means of the linearized theory
- A Brief Hydrodynamic Investigation of a 1/24-Scale Model of the DR-77 Seaplane
- Calculated spanwise lift distributions, influence functions, and influence coefficients for unswept wings in subsonic flow
- A vector study of linearized supersonic flow applications to nonplanar problems
- Reciprocity relations in aerodynamics
- Laminar boundary layer on cone in supersonic flow at large angle of attack
- Displacement effect of a three-dimensional boundary layer
- Diffusion of heat from a line source in isotropic turbulence
- Investigation of a Related Series of Turbine-Blade Profiles in Cascade
- Flight Determination of the Static Longitudinal Stability Boundaries of the Bell X-5 Research Airplane with 59 Deg Sweepback
- Flame velocities of propane- and ethylene-oxygen-nitrogen mixtures
- A flight study of the effects on tracking performance of changes in the lateral-oscillatory characteristics of a fighter airplane
- Flight measurements of the horizontal-tail loads on a swept-wing fighter airplane at transonic speeds
- Free-flight-tunnel investigation of the low-speed stability and control characteristics of a model having a fuselage of relatively flat cross section
- Free-jet investigation of a 20-inch ram-jet combustor utilizing high-heat-release pilot burner
- Techniques for determining thrust in flight for airplanes equipped with afterburners
- Engineering method of ram-jet thrust determination based on experimentally obtained combustor parameters
- Effect of fuel volatility characteristics on ignition-energy requirements in a turbojet combustor
- Investigation of Liquid Fluorine-Liquid Ammonia Propellant Combination in a 100-Pound-Thrust Rocket Engine
- Investigation of a supersonic-compressor rotor with turning to axial direction 1: rotor design and performance