TRAIL - Technical Report Archive and Image Library

Transonic Zero-Lift Drag Tests of Four Equivalent-Body-of-Revolution Models Representing Variations of the Convair F-102 Airplane

Free-Spinning and Recovery Characteristics of a 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning Tunnel

Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair F-102A Airplane at Transonic Speeds

Turbojet Propulsion-System Research and the Resulting Effects on Airplane Performance

Emergency Spin-Recovery Device for the 1/18-Scale Model of the Ryan X-13 Airplane as Determined from Tests in the Langley 20-Foot Free-Spinning Tunnel

Aerodynamic Design of Axial-Flow Compressors. VII - Blade-Element Flow in Annular Cascades

Jet effects on longitudinal trim of an airplane configuration measured at Mach numbers between 1.2 and 1.8

Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination

A transonic wind-tunnel investigation of the longitudinal force and moment characteristics of two delta wings and one clipped-tip delta wing of 4 percent thickness on a slender body

Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions

Loads on thin wings at transonic speeds

A study of means for rationalizing airplane design loads

Landing conditions for large airplanes in routine operations

Some factors affecting the variation of pitching moment with sideslip of aircraft configurations

Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron

Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase against maneuvering and nonmaneuvering targets

Free-flight investigation to determine some effects of tail damping and wing-tail interference on the rolling effectiveness of inboard and outboard ailerons on an untapered sweptback wing

Free-flight investigation, including some effects of wing aeroelasticity, of the rolling effectiveness of an all-movable horizontal tail with differential incidence at Mach numbers from 0.6 to 1.5

Effects of leading-edge radius on the longitudinal stability of two 45 degree sweptback wings as influenced by Reynolds numbers up to 8.20 x 10(exp 6) and Mach numbers up to 0.303

Development of a new flutter testing technique using a towed dynamic airplane model equipped with an automatic stabilizing system: Experimental and calculated dynamic stability characteristics for speeds up to 200 mph

A survey of unclassified axial-flow-compressor literature

Flight measurements of the vertical-tail loads on the Convair XF-92A delta-wing airplane

Effects of sweep and taper on the longitudinal characteristics of an aspect ratio 3 wing-body combination at Mach numbers from 0.6 to 1.4

A method for simulating the atmospheric entry of long-range ballistic missiles

Flight Determination of the Longitudinal Stability and Control Characteristics of a 0.125-Scale Rocket-Boosted Model of the Mcdonnell F-101 Airplane at Mach Numbers from 0.82 to 1.84

An investigation of string support interference on base pressure and forebody chord force at Mach numbers from 0.60 to 1.30

Collection and summary of flap-type-aileron rolling-effectiveness data at zero lift as determined by rocket-powered model tests at Mach numbers between 0.6 and 1.6

The longitudinal characteristics at Mach numbers up to 0.92 of several wing-fuselage-tail combinations having sweptback wings with NACA four-digit thickness distributions

The effect of wing height on the longitudinal characteristics at high subsonic speeds of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and NACA four digit thickness distribution

Icing Limit and Wet-Surface Temperature Variation for Two Airfoil Shapes Under Simulated High-Speed Flight Conditions

A Fibrous-Glass Compact as a Permeable Material for Boundary-Layer-Control Applications Using Area Suction

Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6

NACA Conference on engine stall and surge

Preliminary analysis of performance of turbojet engines used as pumps for boundary-layer control

Variation of Local Liquid-Water Concentration About an Ellipsoid of Fineness Ratio 10 Moving in a Droplet Field

Full-scale, free-jet investigation of methods of improving outlet flow distribution in a side-inlet supersonic diffuser

Impingement of Water Droplets on a Sphere

Impingement of Water Droplets on NACA 65A004 Airfoil at 0 Deg Angle of Attack

Preliminary Data on Rain Deflection from Aircraft Windshields by Means of High-Velocity Jet-Air Blast

An Investigation of the Effects of Nose and Lip Shapes for an Underslung Scoop Inlet at Mach Numbers from 0 to 1.9

Performance Characteristics of Several Divergent-Shroud Aircraft Ejectors

Statistical measurements of contact conditions of 478 transport-airplane landings during routine daytime operations

Free-Spinning-Tunnel Investigation to Determine the Effect of Spin-Recovery Rockets and Thrust Simulation on the Recovery Characteristics of a 1/21-Scale Model of the Chance Vought F7U-3 Airplane, TED No. NACA AD 3103

Free-Spinning-Tunnel Investigation of a 0.034-Scale Model of the Production Version of the Chance Vought F7U-3 Airplane, TED No. NACA AD 3103

Lateral Stability and Control Measurements of a 0.0858-Scale Model of the Lockheed XF-104 Airplane at Transonic Speeds

Altitude Performance of Modified J71 Afterburner with Revised Engine Operating Conditions

An experimental study of applied ground loads in landing

The hydrodynamic characteristics of modified rectangular flat plates having aspect ratios of 1.00, 0.25, and 0.125 and operating near a free water surface

Theoretical and experimental investigation of heat transfer by laminar natural convection between parallel plates

Stress analysis of circular semimonocoque cylinders with cutouts

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