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Effect of nose shape and trailing-edge bluntness on the aerodynamic characteristics of an unswept wing of aspect ratio 3.1, taper ratio 0.4, and 3-percent thickness

Effect of a leading-edge flap upon the lift, drag, and pitching moment of an airplane employing a thin, unswept wing

Effects of diffuser and center-body length on performance of annular diffusers with constant-diameter outer walls and with vortex-generator flow controls

Analysis of rocket, ram-jet, and turbojet engines for supersonic propulsion of long-range missiles 1: rocket-engine performance

Effects of base bleed on the base pressure of blunt-trailing-edge airfoils at supersonic speeds

Free-flight zero-lift drag-rise measurements of equivalent bodies of revolution of several versions of the Douglas XF4D-1 airplane at transonic speeds: TED No. NACA AD 394

Experimental investigation of drag of afterbodies with exiting jet at high subsonic Mach numbers

Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts

Drag and longitudinal trim characteristics of a low-tail version of the North American YF-100A airplane as determined from the flight test at low lift of a 0.11-scale rocket-powered model at Mach numbers between 0.75 and 1.78

Minimum drag of 0.11-scale rocket-powered models of the Chance Vought XF8U-1 airplane, with and without nose modifications, at Mach numbers between 0.85 and 1.30 : TED No. NACA DE 392

A summary of the drag and longitudinal trim at low lift of the North American YF-100A airplane at Mach numbers from 0.75 to 1.77 as determined by flight tests of 0.11-scale rocket models

Altitude investigation of 20-inch-diameter ram-jet engine with annular-piloted combustor

Performance of a vaporizing annular turbojet combustor at simulated high altitudes

Preliminary investigation of an annular turbojet combustor having a catalytic-coated liner

A comparison of the longitudinal aerodynamic characteristics at Mach numbers up to 0.94 of swept back wings having NACA 4-digit or NACA 64A thickness distributions

Summary of some rocket-model investigations of effects of wing aspect ratio and thickness on aileron rolling effectiveness including some effects of spanwise aileron location for sweptback wings with aspect ratio of 8

Some effects of aileron span, aileron chord, and wing twist on rolling effectiveness as determined by rocket-powered model tests and theoretical estimates

Large-scale low-speed wind-tunnel tests of a model having a 60 degree delta horizontal canard control surface and wing to obtain static-longitudinal-stability and canard surface hinge-moment data

Tests of the Northrop XB-62 Missile in the Ames 40- by 80-Foot Wind Tunnel

Longitudinal Aerodynamic Characteristics to Large Angles of Attack of a Cruciform Missile Configuration at a Mach Number of 2

Preliminary Investigation of a Technique for Stability Studies of a Self-Propelled Model of a Submerged Submarine

Investigation of three low-temperature-ratio combustor configurations in a 48-inch-diameter ram-jet engine

A Method for Prevention of Screaming in Rocket Engines

Variation of Local Liquid-Water Concentration About and Ellipsoid of Fineness Ratio 5 Moving in a Droplet Field

Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section

Analysis of rocket, ramjet, turbojet engines for supersonic propulsion of long-range missiles. 2: Rocket missile performance

Analysis of rocket, ramjet, and turbojet engines for supersonic propulsion of long-range missiles. 3: Ramjet engine performance

Combined Compressor Coolant Injection and Afterburning for Turbojet Thrust Augmentation

Pumping Characteristics for Several Simulated Variablegeometry Ejectors With Hot and Cold Primary Flow

Experimental Sea-Level Static Investigation of a Short Afterburner

A theoretical study of the effect of forward speed on the free-space sound-pressure field around propellers

Effect of Ice Formations on Section Drag of Swept NACA 63A-009 Airfoil with Partial-Span Leading-Edge Slat for Various Modes of Thermal Ice Protection

A flight investigation of the practical problems associated with porous-leading-edge suction

Investigation of Noise Field and Velocity Profiles of an Afterburning Engine

Thrust and Pumping Characteristics of a Series of Ejector-type Exhaust Nozzles at Subsonic and Supersonic Flight Speeds

Investigation of an on-off inlet shock-position control on a 16-inch ram-jet engine

The Effect of Blunt-Trailing-Edge Modifications on the High-Speed Stability and Control Characteristics of a Swept-Wing Fighter Airplane

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


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