Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
4176 results returnedSearch results
- Elastic and plastic buckling of simply supported metalite type sandwich plates in compression
- Recommended Values of Meteorological Factors to Be Considered in the Design of Aircraft Ice-Prevention Equipment
- Effect of increase in afterbody length on the hydrodynamic qualities of a flying-boat hull of high length-beam ratio
- A mathematical theory of plasticity based on the concept of slip
- Response of a helicopter rotor to oscillatory pitch and throttle movements
- Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings
- Gust-tunnel investigation of a wing model with semichord line swept back 30 degrees
- The effects of aerodynamic brakes upon the speed characteristics of airplanes
- Direct-reading design charts for 24S-T aluminum-alloy flat compression panels having longitudinal straight-web Y-section stiffeners
- Theoretical analysis of oscillations of a towed cable
- A study of stall phenomena on a 45 degree swept-forward wing
- Overbalancing in residual-liquidation computations
- Comparison of over-all impact loads obtained during seaplane landing tests with loads predicted by hydrodynamic theory
- Flow studies in the asymmetric adjustable nozzle of the Ames 6-by 6-foot supersonic wind tunnel
- Investigation of internal regenerative fuel-heating system for 20-inch ram jet
- Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel IV : the effect of a constant-chord leading-edge flap at high subsonic speeds
- Investigation of extensible wing-tip ailerons on an untapered semispan wing at 0 degree and 45 degrees sweepback
- Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel V : static longitudinal stability and control throughout the subsonic speed range of a semispan model of a supersonic airplane
- The effects of scale and test technique on the validity of small-scale measurements of the aerodynamic characteristics of a wing with the leading edge swept back 63 degrees
- Investigation of a thin straight wing of aspect ratio 4 by the NACA wing-flow method: Lift and pitching-moment characteristics of the wing alone
- Investigations of an annular diffuser-fan combination handling rotating flow
- Investigation of several clamshell variable-area exhaust nozzles for turbojet engines
- Method of determining centrifugal-flow-compressor performance with water injection
- Wing-tunnel investigation at low transonic speeds of the effects of number of wings on the lateral-control effectiveness of an RM-5 test vehicle
- Analysis of measured pressures on airfoils at Mach numbers near 1
- A preliminary experimental investigation of a submerged cascade inlet
- Preliminary experimental investigation of effects of aerodynamic shape of concentrated weights on flutter of a straight cantilever wing
- Preliminary investigation of a variable mass-flow supersonic nose inlet
- Wind-tunnel investigation of transonic aileron flutter
- Preliminary full-scale investigation of a 1/3-scale model of a convertible-type airplane
- Pressure-distribution data for the NACA 64(sub 1)-012 and 64(sub 1) A012 airfoils at high subsonic Mach numbers
- Preliminary Wind-Tunnel Tests of Triangular and Rectangular Wings in Steady Roll at Mach Numbers of 1.62 and 1.92
- Lateral and directional stability and control characteristics of a C-54D airplane
- Determination of rate, area, and distribution of impingement of water drops on various airfoils from trajectories obtained on the differential analyzer
- Vibrational modes of several hollow turbine blades and of solid turbine blade of similar aerodynamic design
- Downwash in vortex region behind trapezoidal-wing tip at Mach number 1.91
- Analytical determination of effect of water injection on power output of turbine-propeller engine
- Aerodynamic characteristics of a wing with quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bumb method
- Carbon deposition from AN-F-58 fuels in a J33 single combustor
- Comparison of effectiveness of coordinated turns and level sideslips for correcting lateral displacement during landing approaches
- Aerodynamic characteristics of a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section: transonic-bump method
- Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section
- The aerodynamic characteristics throughout the subsonic speed range of a thin, sharp-edged horizontal tail of aspect ratio 4 equipped with a constant-chord elevator
- Analysis and experimental observation of pressure losses in ram-jet combustion chambers
- An analysis of a highly compounded two-stroke-cycle compression-ignition engine
- Evaluation of piston-type gas-generator engine for subsonic transport operation.
- Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4
- Effects of systematic changes of trailing-edge angle and leading-edge radius on the variation with Mach number of the aerodynamic characteristics of a 10-percent-chord-thick NACA airfoil section
- Estimated transonic flying qualities of a tailless airplane based on a model investigation
- Estimation of the forces and moments acting on inclined bodies of revolution of high fineness ratio