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- An analysis of shock-wave cancellation and reflection for porous walls which obey an exponential mass-flow pressure-difference relation
- Wall interference in wind tunnels with slotted and porous boundaries at subsonic speeds
- Measurements of pressure and temperature for appraisal of the temperature method of airspeed calibration in the lower stratosphere
- Description and preliminary flight investigation of an instrument for detecting subnormal acceleration during take-off
- Boundary-layer transition at Mach 3.12 with and without single roughness elements
- An investigation of the use of rocket-powered models for gust-load studies with an application to a tailless swept-wing model at transonic speeds
- Considerations on a large hydraulic jet catapult
- Preliminary Altitude Performance Characteristics of the J57-P-1 Turbojet Engine with Fixed-Area Exhaust Nozzle
- Performance of 15-Stage Experimental J71 Axial-Flow Compressor: 2 - Individual Stage Performance Characteristics
- Effect on Drag of Longitudinal Positioning of Half-Submerged and Pylon-Mounted Douglas Aircraft Stores on a Fuselage with and without Cavities between Mach Numbers 0.9 and 1.8
- Permeability and Strength Measurements on Sintered, Porous, Hollow Turbine Blades Made by the American Electro Metal Corporation under Office of Naval Research Contract N-ONR-295 (01)
- Experimental Permeability Measurements on a Strut-Supported Transpiration-Cooled Turbine Blade with Stainless-Steel Shell made by the Federal-Mogul Corporation under Bureau of Aeronautics Contract N0as 51613-C
- Summary of Free-Flight Zero-Lift Drag Results from Tests of 1/5-Scale Models of the Convair YF-102 and F-102A Airplanes and Several Related Small Equivalent Bodies at Mach Numbers from 0.70 to 1.46
- Free-Flight Zero-Lift Drag Results from a 1/5-Scale Model and Several Small-Scale Equivalent Bodies of Revolution of the Convair F-102 Configuration at Mach Numbers up to 1.34
- A note on secondary flow in rotating radial channels
- Determination of mean camber surfaces for wings having uniform chordwise loading and arbitrary spanwise loading in subsonic flow
- An analytical study of the effect of airplane wake on the lateral dispersion of aerial sprays
- An air-flow-direction pickup suitable for telemetering use on pilotless aircraft
- A comparative analysis of the performance of long-range hypervelocity vehicles
- Behavior of materials under conditions of thermal stress
- An experimental investigation of reduction in transonic drag rise at zero lift by the addition of volume to the fuselage of a wing-body-tail configuration and a comparison with theory
- Experimental investigation of effects of primary jet flow and secondary flow through a zero-length ejector on base and boattail pressures of a body of revolution at free-stream Mach numbers of 1.62, 1.93, and 2.41
- Stability and Control Flight Tests of a Vertically Rising Airplane Model Similar to the Lockheed XFV-1 Airplane
- Studies of the lateral-directional flying qualities of a tandem helicopter in forward flight
- Effects of Fuselage Modifications on the Drag Characteristics of a 1/20-Scale Model of the Convair F-102 Airplane at Transonic Speeds
- Preliminary Low-Speed Wind-Tunnel Investigation of Some Aspects of the Aerodynamic Problems Associated with Missiles Carried Externally in Positions Near Airplane Wings
- Investigation of the Hydrodynamic Characteristics of the Panto-Base Chase C-123 Airplane
- Preliminary Altitude Performance Data of J71-A2 Turbojet Engine Afterburner
- Preliminary Altitude Performance Data for the J71-A2 (X-26) Turbojet Engine
- Theoretical study of the transonic lift of a double-wedge profile with detached bow wave
- A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers
- The zero-lift drag of a slender body of revolution (NACA RM-10 research model) as determined from tests in several wind tunnels and in flight at supersonic speeds
- Unsteady oblique interaction of a shock wave with a plane disturbance
- A method of measuring jet thrust of turbojet engines in flight installations
- Effect of horizontal-tail span and vertical location on the aerodynamic characteristics of an unswept tail assembly in sideslip
- Formation and combustion of smoke in laminar flames
- Convection of a pattern of vorticity through a shock wave
- Low-Speed Longitudinal Stability and Lateral-Control Characteristics of a 0.3-Scale Model of the Republic RF-84F Airplane at a Reynolds Number of 9x10(exp 6)
- Effect of ground interference on the aerodynamic and flow characteristics of a 42 degree sweptback wing at Reynolds numbers up to 6.8 x 10(6)
- Exact solutions of laminar-boundary-layer equations with constant property values for porous wall with variable temperature
- A study of the characteristics of human-pilot control response to simulated aircraft lateral motions
- Structural response to discrete and continuous gusts of an airplane having wing bending flexibility and a correlation of calculated and flight results
- A visualization study of secondary flows in cascades
- Experimental investigation of acceleration characteristics of a turbojet engine including regions of surge and stall for control applications
- Comparison of performance of experimental and conventional cage designs and materials for 75-millimeter-bore cylindrical roller bearings at high speed
- Effects of sweep and thickness on the static longitudinal aerodynamic characteristics of a series of thin, low-aspect-ratio, highly tapered wings at transonic speeds: transonic-bump method
- Wind-tunnel investigation at low speed of the effects of chordwise wing fences and horizontal-tail position on the static longitudinal stability characteristics of an airplane model with a 35 degree sweptback wing
- Wind-Tunnel Investigation at Subsonic and Supersonic Speeds of a Fighter Model Employing a Low-aspect-ratio Unswept Wing and a Horizontal Tail Mounted Well above the Wing Plane - Lateral and Directional Stability
- Effect of a Leading-edge Flap upon the Lift, Drag, and Pitching Moment of an Airplane Employing a Thin, Unswept Wing
- Longitudinal Stability Characteristics of the Consolidated Vultee XFY-1 Airplane with Windmilling Propellers as Obtained from Flight of 0.133-Scale Rocket-Propelled Model at Mach Numbers from 0.70 to 1.13