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Analytical determination of the natural coupled frequencies and mode shapes and the response to oscillating forcing functions of tandem helicopters

Transition-flight tests of a model of a low-wing transport vertical-take-off airplane with tilting wing and propellers

Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by a free-oscillation method

Aerodynamic design of axial-flow compressors Volume 1

Bending tests of ring-stiffened circular cylinders

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

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

Bodies of revolution having minimum drag at high supersonic airspeeds

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

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 interference effects of lateral-support struts on afterbody pressures at Mach 1.9

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


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