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- A bibliography of NACA reports on control of turbojet engines
- The Compressible Laminar Boundary Layer with Heat Transfer and Arbitrary Pressure Gradient
- Component performance investigation of J71 experimental turbine VI : effect of first-stator adjustment; over-all performance of J71-97 turbine with 70-percent-design stator area
- Component performance investigation of J71 experimental turbine VIII : effect of first-stator adjustment; internal flow conditions of J71-97 turbine with 70-percent-design stator area
- Analysis of elastic thermal stresses in thin plate with spanwise and chordwise variations of temperature and thickness
- Analysis of laminar incompressible flow on semiporous channels
- Analysis of a flight investigation at supersonic speeds of a simple homing system
- Bodies of revolution having minimum drag at high supersonic airspeeds
- The change with mass-flow ratio of the cowl pressure drag of normal-shock inlets at supersonic speeds
- Component performance of J71-A-2(600-D1) turbojet engine at several Reynolds number indices
- Compressive stress-strain properties of 2024-T3 aluminum-alloy sheet at elevated temperatures
- Compressive and torsional buckling of thin-wall cylinders in yield region
- Compressive stress-strain properties of 7075-T6 aluminum-alloy sheet at elevated temperatures
- Analysis of an automatic control to prevent rolling divergence
- Boundary layer behind shock or thin expansion wave moving into stationary fluid
- Boundary-layer transition at supersonic speeds
- Effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces
- Experimental and analytical investigation of an acceleration regulating control for a turbojet engine
- Determination of vortex paths by series expansion technique with application to cruciform wings
- A simplified method for evaluating jet-propulsion-system components in terms of airplane performance
- Free-flight measurements of the zero-lift drag of several wings at Mach numbers from 1.4 to 3.8
- Effect of transverse body force on channel flow with small heat addition
- Effect of wing size and amount of indentation on applicability of transonic area rule to swept-wing configurations
- Effectiveness of inhibitors for mass transfer and corrosion in sodium hydroxide - nickel systems
- Experimental investigation of interference effects of lateral-support struts on afterbody pressures at Mach 1.9
- Effects of internal boundary-layer control on the performance of supersonic aft inlets
- The effect of fluid injection on the compressible turbulent boundary layer : the effect of skin friction of air injected into the boundary layer of a cone at M = 2.7
- An evaluation of an aeromechanical method of minimizing servo- missile transfer function variations with flight condition
- Evaluation of an automatic inlet-pressure control valve for study of transient engine performance characteristics
- Effects of vertical fins near the nose of the fuselage on the directional and damping-in-yaw stability derivatives of an airplane model under steady-state and oscillatory conditions
- The Effects of the Addition of Small Fuselage-Mounted Fins on the Static Directional Stability Characteristics of a Model of a 45 Degree Swept-Wing Airplane at Angles of Attack up to 15.3 degrees at a Mach Number of 2.01
- Effects of variations in combustion-chamber configuration on ignition delay in a 50-pound-thrust rocket
- Experimental investigation of effect of cooling air on turbine performance of two turbojet engines modified for air-cooling
- Experimental investigation of the effect of boundary-layer transition on the average heat transfer to a yawed cylinder in supersonic flow
- Experimental investigation of the aerodynamic loading on a helicopter rotor blade in forward flight
- Aerodynamic characteristics of a 6-percent-thick symmetrical circular-arc airfoil having a 30-percent-chord trailing-edge flap at a Mach number of 6.9
- Tabulated pressure data for a series of controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01
- Tabulated pressure data for several flap-type trailing edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01
- Tables and charts for thermodynamic calculations involving air and fuels containing boron, carbon, hydrogen, and oxygen
- Static stability characteristics of a cambered-delta-wing model at high subsonic speeds
- Static-thrust characteristics of the NACA 8.75-(5)(05)-037 dual-rotation propeller
- A summary of results obtained during flight simulation of several aircraft prototypes with variable-stability airplanes
- Supersonic-area-rule design and rocket-propelled flight investigation of a zero-lift straight-wing-body-nacelle configuration between Mach numbers 0.8 and 1.53
- Self shielding in rectangular and cylindrical geometries
- Shear strength at 75 F to 500 F of fourteen adhesives used to bond a glass-fabric-reinforced phenolic resin laminate to steel
- A simple method for calculating the characteristics of the Dutch roll motion of an airplane
- Some observations on maximum pressure rise across shocks without boundary-layer separation on airfoils at transonic speeds
- Some interference effects that influence vertical-tail loads at supersonic speeds
- A study of fuel-nitric acid reactivity
- A study of a symmetrical, circular, internal, compression inlet