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Wind-Tunnel Investigation of the Low-Speed Static Longitudinal Characteristics of the Republic RF-84F Airplane

Tank Investigation of the Grumman JRF-5 Airplane Equipped with Twin Hydro-Skis: TED No. NACA DE 357

Time Variation of the Distance Separating Bomb and Dive Bomber Subsequent to Bomb Release

Free-Spinning-Tunnel Investigation of a 1/24-Scale Model of the Grumman F9F-6 Airplane: TED No. NACA DE 364

Thrust Augmentation of a Turbojet Engine at Simulated Flight Conditions by Introduction of a Water-Alcohol Mixture into the Compressor

Hydrocarbon and nonhydrocarbon derivatives of cyclopropane

The dynamic-response characteristics of a 35 degree swept-wing airplane as determined from flight measurements

Dynamic response at altitude of a turbojet engine with variable area exhaust nozzle

Flight investigation of a mechanical feel device in an irreversible elevator control system of a large airplane

Theoretical and experimental investigation of mufflers with comments on engine-exhaust muffler design

Theoretical symmetric span loading due to flap deflection for wings of arbitrary plan form at subsonic speeds

Effect of initial mixture temperature on flame speed of methane-air, propane-air, and ethylene-air mixtures

Two-and three-dimensional unsteady lift problems in high-speed flight

Flight investigation of the effect of control centering springs on the apparent spiral stability of a personal-owner airplane

Force Characteristics in the Submerged and Planing Condition of a 1/5.78-Scale Model of a Hydro-Ski-Wheel Combination for the Grumman JRF-5 Airplane

Effect of aspect ratio on the low-speed lateral control characteristics of untapered low-aspect-ratio wings equipped with flap and with retractable ailerons

The effects on dynamic lateral stability and control of large artificial variations in the rotary stability derivatives

An Investigation of the Effects of a Vortex-Generator Configuration on the Aerodynamic Characteristics of a 1/4-Scale Model of the X-1 Airplane (10-Percent-Thick Wing)

Axisymmetric supersonic flow in rotating impellers

Effects of compressibility on the performance of two full-scale helicopter rotors

Discussion of boundary-layer characteristics near the wall of an axial-flow compressor

Flight Characteristics of a 1/4-Scale Model of the XFV-1 Airplane (TED No. NACA DE-378)

Control characteristics at transonic speeds of a linked flap and spoiler on a tapered 45 degrees sweptback wing of aspect ratio 3

Investigation of engine performance and high-temperature properties of precision-cast turbine blades of high carbon Stellite 21 and controlled grain-size-Stellite 21

Investigation of flow fluctuations at the exit of a radial-flow centrifugal impeller

Aerodynamic characteristics at transonic speeds of a tapered 45 degree sweptback wing of aspect ratio 3 having a full-span flap type of control with overhang balance : transonic-bump method

Flight determination of the longitudinal stability of a 1/10-scale rocket-powered model of the Northrop MX-775A missile at low lift coefficients and Mach numbers from 0.89 to 1.34

Effects of the spanwise, chordwise and vertical location of an external store on the aerodynamic characteristics of a 60 degree delta wing at Mach numbers of 1.41, 1.62, and 1.96

Control characteristics of trailing-edge spoilers on untapered blunt trailing-edge wings of aspect ratio 2.7 with 0 degree and 45 degrees sweepback at Mach numbers of 1.41 and 1.96

Effects of systematically varying the spanwise and vertical location of an external store on the aerodynamic characteristics of an unswept tapered wing of aspect ratio 4 at Mach numbers of 1.41, 1.62, and 1.96

Full-scale wind-tunnel investigation of the effects of wing modifications and horizontal-tail location on the low-speed static longitudinal characteristics of a 35 degree swept-wing airplane

Investigation of lift and center of pressure of low-aspect-ratio, cruciform, triangular, and rectangular wings in combination with a slender fuselage at high supersonic speeds

Investigation of performance of several double-shroud ejectors and effect of variable-area exhaust nozzle on single ejector performance

Investigation of power extraction characteristics and braking requirements of a windmilling turbojet engine

Investigation of losses in the XJ35-A-23 two-stage turbine

Investigation of internal film cooling of exhaust nozzle of a 1000-pound-thrust liquid-ammonia liquid-oxygen rocket

Investigation of a 10-stage subsonic axial-flow research compressor I : aerodynamic design

Investigation of heat-transfer coefficients in an afterburner

Wing load distribution on a swept wing airplane in flight at Mach numbers up to 1.11, and comparison with theory

Variation of pressure limits of flame propagation with tube diameter for various isooctane-oxygen-nitrogen mixtures

Comparison between prediction and experiment for all-movable wing and body combinations at supersonic speeds - drag due to lift and lift-drag ratio

Instrumentation and calibration technique for flight calibration of angle-of-attack systems on aircraft

Instrumentation of the Ames supersonic free-flight wind tunnel

Investigation of thrust augmentation using water-alcohol injection on a 5200-pound-thrust axial-flow-type turbojet engine at static sea-level conditions

Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor tip-speed II : velocity-diagram study of turbine for engine operation with constant exhaust-nozzle area

Investigation of stresses due to thermal gradients in typical aircraft structures

Investigation of vanes immersed in the jet of a solid-fuel rocket motor

Investigations of air-cooled turbine rotors for turbojet engines 2: mechanical design, stress analysis, and burst test of modified J33 split-disk rotor

Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed III : velocity-diagram study of two-stage and downstream-stator turbines for engine operation at constant rotative speed

Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor-tip speed I : turbine-design requirements for several engine operating conditions


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