Browse TRAIL Inventories

Charts of boundary-layer mass flow and momentum for inlet performance analysis mach number range, 0.2 to 5.0

On the calculation of the 1 (center dot) P oscillating aerodynamic loads on single-rotation propellers in pitch on tractor airplanes

A flight evaluation of the longitudinal stability characteristics associated with the pitch-up of a swept-wing airplane in maneuvering flight at transonic speeds

Performance of 15-Stage Experimental J71 Axial-Flow Compressor. 3 - Effects of Inlet-Guide-Vane Adjustment

Investigation of the vibrations of a hollow thin-walled rectangular beam

A method for the design of sweptback wings warped to produce specified flight characteristics at supersonic speeds

NACA transonic wind-tunnel test sections

Measurement and analysis of wing and tail buffeting loads on a fighter airplane

Ideal temperature rise due to constant-pressure combustion of a JP-4 fuel

On the Kernel function of the integral equation relating the lift and downwash distributions of oscillating finite wings in subsonic flow

Determination of lateral-stability derivatives and transfer-function coefficients from frequency-response data for lateral motions

Longitudinal Aerodynamic Characteristics and Effect of Rocket Jet on Drag of Models of the Hermes A-3A and A-3B Missiles in Free Flight at Mach Numbers From 0.6 to 2.0

A comparative analysis of the performance of long-range hypervelocity vehicles

Bodies of revolution having minimum drag at high supersonic airspeeds

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

Tank investigation of the hydrodynamic characteristics of a 1/13.33-scale jet-powered dynamic model of the Martin XP6M-1 flying boat: TED No. NACA DE 385

Minimum-drag ducted and pointed bodies of revolution based on linearized supersonic theory

Development of craze and impact resistance in glazing plastics by multiaxial stretching

Comparison of the Drag of a Fin-Stabilized Body of Revolution and of a Complete Airplane Configuration as Obtained at Transonic Speeds in a Slotted Wind Tunnel and in Free Flight

An experimental investigation of the hinge-moment characteristics of a constant-chord control surface oscillating at high frequency

An investigation of the effects of heat transfer on boundary-layer transition on a parabolic body of revolution (NACA RM-10) at a Mach number of 1.61

On boattail bodies of revolution having minimum wave drag

Generalized indical forces on deforming rectangular wings in supersonic flight

Analog study of interacting and noninteracting multiple-loop control systems for turbojet engines

Wind-Tunnel Investigation at Low Speed of the Rolling Stability Derivatives of a 1/10-Scale Model of the Grumman F9F-9 Airplane, TED No. NACA AD 3109

Temperature in a J47-25 Turbojet-Engine Combustor and Turbine Sections During Steady-State and Transient Operation in a Sea-Level Test Stand

Investigation of the compressive strength and creep lifetime of 2024-T3 aluminum-alloy plates at elevated temperatures

Charts for estimating tail-rotor contribution to helicopter directional stability and control in low-speed flight

Error in airspeed measurement due to the static-pressure field ahead of an airplane at transonic speeds

Theoretical analysis of incompressible flow through a radial-inlet centrifugal impeller at various weight flows

Flight Test of the Lateral Stability of a 0.133-Scale Model of the Convair XFY-1 Airplane with Windmilling Propellers at Mach Numbers from 0.70 to 1.12 (TED No. NACA DE 369)

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

An analysis of once-per-revolution oscillating aerodynamic thrust loads on single-rotation propellers on tractor airplanes at zero yaw

Flight experience with two high-speed airplanes having violent lateral-longitudinal coupling in aileron rolls

A flight and analog computer study of some stabilization and command networks for an automatically controlled interceptor during the final attack phase

Flight determination of minimum drag of 0.11-scale rocket-boosted model of the Chance Vought XF8U-1 airplane with modified fuselage area distribution and faired inlet at Mach number from 0.82 to 1.68 : TED No. NACA DE 392

Exploratory investigation at Mach number 4.06 of an airplane configuration having a wing of trapezoidal form : effects of various tail arrangements on wing-on and wing-off static longitudinal and lateral stability characteristics

Exploratory investigation of the flow in the separated region ahead of two blunt bodies at Mach number 2

Flight measurements of the dynamical longitudinal stability and frequency-response characteristics of the XF-92A delta-wing airplane

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

Flight experience with a delta-wing airplane having violent lateral-longitudinal coupling in aileron rolls

Flight measurements of the velocity distribution and persistence of the trailing vortices of an airplane


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