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- Pilot's loss of orientation in inverted spins
- Some effects of system nonlinearities in the problem of aircraft flutter
- Temperature-composition limits of spontaneous explosion for nine alkylsilanes with air at atmospheric pressure
- A technique utilizing rocket-propelled test vehicles for the measurement of the damping in roll of sting-mounted models and some initial results for delta and unswept tapered wings
- Study of the momentum distribution of turbulent boundary layers in adverse pressure gradients
- Analysis of two-dimensional compressible-flow loss characteristics downstream of turbomachine blade rows in terms of basic boundary-layer characteristics
- Analytic determination of the discharge coefficients of flow nozzles
- Use of nonlinearities to compensate for the effects of a rate-limited servo on the response of an automatically controlled aircraft
- Approximate method for determining equilibrium operation of compressor component of turbojet engine
- Turbulent-heat-transfer measurements at a Mach number of 1.62
- Vortex interference on slender airplanes
- Visualization study of secondary flows in turbine rotor tip regions
- Experimental investigation at low speed of effects of fuselage cross section on static longitudinal and lateral stability characteristics of models having 0 and 45 degrees sweptback surfaces
- Generalization of gas-flow-interferometry theory and interferogram evaluation equations for one-dimensional density fields
- Hydrodynamic pressure distributions obtained during a planing investigation of five related prismatic surfaces
- Hydrodynamic tares and interference effects for a 12-percent-thick surface-piercing strut and an aspect-ratio-0.25 lifting surface
- Method of controlling stiffness properties of a solid-construction model wing
- Correction of additional span loadings computed by the Weissinger seven-point method for moderately tapered wings of high aspect ratio
- Analysis of ear formation in deep-drawn cups
- Effect of some selected heat treatments on the operating life of cast HS-21 turbine blades
- A comparison of the measured and predicted lateral oscillatory-characteristics of a 35 degree swept-wing fighter airplane
- Effect of lag of sidewash on the vertical-tail contribution to oscillatory damping in yaw of airplane models
- Application of the generalized shock-expansion method to inclined bodies of revolution traveling at high supersonic airspeeds
- Low-speed static lateral and rolling stability characteristics of a series of configuration composed of intersecting triangular plan-form surfaces
- Free-flight measurements of turbulent-boundary-layer skin friction in the presence of severe aerodynamic heating at Mach numbers from 2.8 to 7.0
- Lift hysteresis at stall as an unsteady boundary-layer phenomenon
- Reduction of profile drag at supersonic velocities by the use of airfoil sections having a blunt trailing edge
- A reevaluation of gust-load statistics for applications in spectral calculations
- Review of Experimental Investigations of Liquid-Metal Heat Transfer
- Wind-tunnel investigation at low speed of effect of size and position of closed air ducts on static longitudinal and static lateral stability characteristics of unswept-midwing models having wings of aspect ratio 2, 4, and 6
- Calculated spanwise lift distributions and aerodynamic influence coefficients for swept wings in subsonic flow
- Axially symmetric shapes with minimum wave drag
- Boundary lubrication of steel with fluorine- and chlorine-substituted methane and ethane gases
- Variation of boundary-layer transition with heat transfer on two bodies of revolution at a Mach number of 3.12
- On spectral analysis of runway roughness and loads developed during taxiing
- Recovery and time-response characteristics of six thermocouple probes in subsonic and supersonic flow
- Calculation of the supersonic pressure distribution on a single-curved tapered wing in regions not influenced by the root or tip
- Extrapolation techniques applied to matrix methods in neutron diffusion problems
- Theoretical analysis of incompressible flow through a radial-inlet centrifugal impeller at various weight flows II : solution in leading-edge region by relaxation methods
- Gust-tunnel investigation of the effect of a sharp-edge gust on the flapwise blade bending moments of a model helicopter rotor
- Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load
- Circumferential distribution of propeller-slipstream total-pressure rise at one radial station of a twin-engine transport airplane
- An experimental investigation of regions of separated laminar flow
- Theoretical analysis of incompressible flow through a radial-inlet centrifugal impeller at various weight flows 1: solution by a matrix method and comparison with an approximate method
- An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of Riveted Connection Between Sheet and Stringer
- A limited investigation of the effect of three vortex-generator configuration on the effectiveness of a plain flap on an unswept wing
- Flow studies on flat-plate delta wings at supersonic speed
- On slender delta wings with leading-edge separation
- A study of boundary-layer transition and surface temperature distributions at Mach 3.12
- The effectiveness of wing vortex generators in improving the maneuvering characteristics of a swept wing airplane at transonic speeds