Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
4176 results returnedSearch results
- Quantitative analysis of ternary mixtures of naphthalene, 1-methylnaphthalene, and 2-methylnaphthalene by ultraviolet spectrophotometry
- Stability derivatives of triangular wings at supersonic speeds
- Stability derivatives of thin rectangular wings at supersonic speeds : wing diagonal ahead of tip mach lines
- An analysis of the airspeeds and normal accelerations of Sikorsky S-42A airplanes in commercial transport operation
- High-speed wind-tunnel investigation of an NACA 65-210 semispan wing equipped with plug and retractable ailerons and a full-span slotted flap
- The Development of Cambered Airfoil Sections Having Favorable Lift Characteristics at Supercritical Mach Numbers
- Development of cast aluminum alloys for elevated-temperature service
- An analysis of the airspeeds and normal accelerations of Martin M-130 airplanes in commercial transport operation
- Control considerations for optimum power proportionment in turbine-propeller engines
- Effect of taper ratio on low-speed static and yawing stability derivatives of 45 degree sweptback wings with aspect ratio of 2.61
- Influence of leading-edge suction on lift-drag ratios of wings at supersonic speeds
- An analysis of the airspeed and normal accelerations of Douglas DC-2 airplanes in commercial transport operation
- An analysis of the airspeeds and normal accelerations of Boeing B-247 and B-247D airplanes in commercial transport operation
- Fatigue strength and related characteristics of aircraft joints 2: fatigue characteristics of sheet and riveted joints of 0.040-inch 24S-T, 75S-T, and R303-T275 aluminum alloys
- An experimental investigation of an NACA 631-012 airfoil section with leading-edge suction slots
- Jet diffuser for simulating ram-pressure and altitude conditions on a turbojet-engine static test stand
- A metallurgical investigation of a contour-forged disc of EME alloy
- A metallurgical investigation of two contour forged gas-turbine discs of 19-9DL alloy
- A metallurgical investigation of five forged gas-turbine discs of Timken alloy
- A metallurgical investigation of two large discs of CSA alloy
- A metallurgical investigation of two turbosupercharger discs of 19-9DL alloy
- A method for determination of aromatics in 150 degree to 300 degree C fractions of crude petroleum by measurement of aniline-point rise
- Investigation of boundary-layer Reynolds number for transition on an NACA 65(215)-114 airfoil in the Langley two-dimensional low-turbulence pressure tunnel
- Experimental and calculated characteristics of several high-aspect-ratio tapered wings incorporating NACA 44-series, 230-series, and low-drag 64- series airfoil sections
- Jet-boundary-induced-upwash velocities for swept reflection-plane models mounted vertically in 7- by 10-foot, closed, rectangular wind tunnels
- Stresses in and general instability of monocoque cylinders with cutouts V : calculation of the stresses in cylinders with side cutout
- Structural evaluation of an extruded magnesium-alloy T-stiffened panel
- Stresses in and general instability of monocoque cylinders with cutouts IV : pure bending tests of cylinders with side cutout
- Stresses in and general instability of monocoque cylinders with cutouts VI : calculation of the buckling load of cylinders with side cutout subjected to pure bending
- Analytical and experimental performance of an explosion-cycle combustion chamber for a jet-propulsion engine
- The use of source-sink and doublet distributions extended to the solution of boundary value problems in supersonic flow
- Approximate relations for hinge-moment parameters of control surfaces on swept wings at low Mach numbers
- An approximate determination of the lift of slender cylindrical bodies and wing-body combinations at very high supersonic speeds
- Flight tests of an apparatus for varying dihedral effect in flight
- Investigation of the penetration on an air jet directed perpendicularly to an air stream
- Effect of size and number of outlet pipes on design of collectors for rating and testing axial-flow compressors
- Effects of compressibility on the flow past thick airfoil sections
- Cylinder-temperature and cooling-air-pressure instrumentation for air-cooled-engine cooling investigations
- The damping due to roll of triangular, trapezoidal, and related plan forms in supersonic flow
- An application of Falkner's surface-loading method to predictions of hinge-moment parameters for swept-back wings
- Application of the linearized theory of supersonic flow to the estimation of control-surface characteristics
- Charts for the conical part of the downwash field of swept wings at supersonic speeds
- The effects of compressibility on the lift, pressure, and load characteristics of a tapered wing of NACA 66-series airfoil sections
- Wind-tunnel investigation of boundary-layer control by suction on NACA 655-424 airfoil with double slotted flap
- Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan wing model
- The calculation of downwash behind supersonic wings with an application to triangular plan forms
- Calculation of the effect of thrust-axis inclination on propeller disk loading and comparison with flight measurements
- Buckling in shear of continuous flat plates
- Buckling stresses of clamped rectangular flat plates in shear
- The design of low-turbulence wind tunnels