Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
7169 results returnedSearch results
- Effect of an autopilot sensitive to yawing velocity on the lateral stability of a typical high-speed airplane
- Fluctuations in a spray formed by two impinging jets
- Further comparisons of theoretical and experimental lift and pressure distributions on airfoils in cascade at low-subsonic speed
- Fundamental effects of cold-working on creep properties of low-carbon N-155 alloy
- Infrared spectra of 59 dicyclic hydrocarbons
- Investigation of NACA 64,2-432 and 64,3-440 airfoil sections with boundary-layer control and an analytical study of their possible applications
- A method of designing turbomachine blades with a desirable thickness distribution for compressible flow along an arbitrary stream filament of revolution
- A method for the determination of the spanwise load distribution of a flexible swept wing at subsonic speeds
- Method of analysis for compressible flow arbitrary turbomachine blades on general surface of revolution
- Lift and moment on oscillating triangular and related wings with supersonic edges
- Floating characteristics of a plain and a horn-balanced rudder at spinning attitudes as determined from rotary tests on a model of a typical low-wing personal-owner airplane
- Full-scale-tunnel investigation of the static-thrust performance of a coaxial helicopter rotor
- Friction at high sliding velocities of oxide films on steel surfaces boundary-lubricated with stearic-acid solutions
- Heat transfer to bodies in a high-speed rarefied-gas stream
- On the second-order tunnel-wall-constriction corrections in two-dimensional compressible flow
- On the use of coupled modal functions in flutter analysis
- On two-dimensional flow after a curved stationary shock (with special reference to the problem of detached shock waves)
- Effect of fuel immersion on laminated plastics
- A critical review of notch sensitivity in stress-rupture tests
- Criterions for condensation-free flow in supersonic tunnels
- Analytical evaluation of aerodynamic characteristics of turbines with nontwisted rotor blades
- Analysis of pure-bending flutter of a cantilever swept wing and its relation to bending-torsion flutter
- An analytical investigation of effect of high-lift flaps on take-off of light airplanes
- Bench-test investigation of the transient-response characteristics of several simulated airplanes incorporating an autopilot sensitive to yawing accelerations
- Effect of various parameters including Mach number on the single-degree-of-freedom flutter of a control surface in potential flow
- Effectiveness of ceramic coatings in reducing corrosion of five heat-resistant alloys by lead-bromide vapors
- The effect of rate of change of angle of attack on the maximum lift coefficient of a pursuit airplane
- An experimental determination of the critical bending moment of a box beam stiffened by posts
- An experimental investigation of the effect of surface heating on boundary-layer transition on a flat plate in supersonic flow
- Tables of exact laminar-boundary-layer solutions when the wall is porous and fluid properties are variable
- A procedure for calculating the development of turbulent boundary layers under the influence of adverse pressure gradients
- Some measurements of the effect of gaseous imperfections on the critical pressure ratio in air and the speed of sound in nitrogen
- A study of elastic and plastic stress concentration factors due to notches and fillets in flat plates
- Static and fatigue strengths of high-strength aluminum-alloy bolted joints
- A self-synchronizing stroboscopic Schlieren system for the study of unsteady air flows
- Synthesis of cyclopropane hydrocarbons from methylcyclopropyl ketone 3: 2-cyclopropyl-1-butene, cis and trans 2-cyclopropyl-2-butene, and 2-cyclopropylbutane
- Synthesis, purification and physical properties of hydrocarbons of the naphthalene series 1: 1-methylnaphthalene, 1-ethylnaphthalene, 1-butylnaphthalene, and 1-isobutylnaphthalene
- An improved approximate method for calculating lift distributions due to twist
- Experimental study of an angle-of-attack vane mounted ahead of the nose of an airplane for use as a sensing device for an acceleration alleviator
- Flight investigation of some factors affecting the critical tail loads on large airplanes
- Flight investigation of the effect of transient wing response on wing strains of a twin-engine transport airplane in rough air
- General plastic behavior and approximate solutions of rotating disk in strain-hardening range
- An investigation of aircraft heaters XXXVIII : determination of thermal performance of rectangular- and trapezoidal-shaped inner-skin passages for anti-icing systems
- The Indicial Lift and Pitching Moment for a Sinking or Pitching Two-Dimensional Wing Flying at Subsonic or Supersonic Speeds
- Inelastic column behavior
- Theoretical characteristics of two-dimensional supersonic control surfaces
- Theoretical force and moments due to sideslip of a number of vertical tail configurations at supersonic speeds
- Two axial-symmetry solutions for incompressible flow through a centrifugal compressor with and without inducer vanes
- Unsteady laminar boundary-layer flow
- The use of an uncalibrated cone for determination of flow angles and Mach numbers at supersonic speeds