Browse TRAIL Inventories

Matrix method of determining the longitudinal-stability coefficients and frequency response of an aircraft from transient flight data

Measurements of average heat-transfer and friction coefficients for subsonic flow of air in smooth tubes at high surface and fluid temperatures

General algebraic method applied to control analysis of complex engine types

Determination of plate compressive strengths at elevated temperatures

The aerodynamic forces on slender plane- and cruciform-wing and body combinations

Analysis of spanwise temperature distribution in three types of air-cooled turbine blade

Blockage corrections for three-dimensional-flow closed-throat wind tunnels, with consideration of the effect of compressibility

Effect on longitudinal stability and control characteristics of a Boeing B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system

The effects of variations in Reynolds number between 3.0 x 10sub6 and 25.0 x 10sub6 upon the aerodynamic characteristics of a number of NACA 6-series airfoil sections

Performance of J33-A-27 Turbojet-Engine Compressor, III, Over-All Performance Characteristics of Modified Compressor with Water Injection at Design Equivalent Speed of 11,800 RPM

Effect of an Autopilot Sensitive to Yawing Velocity on the Lateral Stability of the Douglas D-558-II Airplane

Results of the Flight Test of a Dummy of the MX-656 Rocket-Propelled Models

Some theoretical low-speed span loading characteristics of swept wings in roll and sideslip

Preliminary Performance Data on General Electric Integrated Electronic Control Operating on J47 RX1-3 Turbojet Engine in NACA Altitude Wind Tunnel

Investigation of Performance of Axial-Flow Compressor of XT-46 Turbine-Propeller Engine 2 - Performance of Revised Compressor at Design Equivalent Speed

Investigation of Performance of Axial-Flow Compressor of XT-46 Turbine-Propeller Engine 1 - Preliminary Investigation at 50-,70-, and 100-Percent Design Equivalent Speed

Data from Tests of a 1/5-Scale Model of a Proposed High-Speed Submarine in the Langley Full-Scale Tunnel

Inelastic column behavior

Theoretical comparison of several methods of thrust augmentation for turbojet engines

Two-dimensional compressible flow in centrifugal compressors with straight blades

Performance of 24-inch supersonic axial-flow compressor in air. III : compressor performance with inlet guide vanes

Automatic control systems satisfying certain general criterions on transient behavior

An introduction to the physical aspects of helicopter stability

Method for calculating lift distributions for unswept wings with flaps or ailerons by use of nonlinear section lift data

Flight investigation of the effect of various vertical-tail modifications on the directional stability and control characteristics of a propeller-driven fighter airplane

Flutter of a uniform wing with an arbitrarily placed mass according to a differential-equation analysis and a comparison with experiment

Analysis of temperature distribution in liquid-cooled turbine blades

The application of Green's theorem to the solution of boundary-value problems in linearized supersonic wing theory

Effect of Various Modifications on Drag and Longitudinal Stability and Control Characteristics at Transonic Speeds of a Model of the XF7U-1 Tailless Airplane: NACA Wing-FLow Method, TED No. NACA DE 307

The reversibility theorem for thin airfoils in subsonic and supersonic flow

The calculation of downwash behind supersonic wings with an application to triangular plan forms

Theoretical analysis of various thrust-augmentation cycles for turbojet engines

Elastic and plastic buckling of simply supported solid-core sandwich plates in compression

Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings

Amplitude distribution and energy balance of small disturbances in plate flow

Summary of the Aerodynamic Characteristics and Flying Qualities Obtained from Flights of Rocket-Propelled Models of an Airplane Configuration Incorporating a Sweptback Inversely Tapered Wing at Transonic and Low-Supersonic Speeds

Analysis of thrust augmentation of turbojet engines by water injection at compressor inlet including charts for calculating compression processes with water injection

Investigation at high subsonic speeds of a 45 sweptback horizontal tail with plain and horn-balanced control surfaces

Further experimental studies of area suction for the control of the laminar boundary layer on a porous bronze NACA 64A010 airfoil

Low-speed investigation of a 0.16-scale model of the X-3 airplane : longitudinal characteristics

Linearized compressible-flow theory for sonic flight speeds

Low-speed tests of a model simulating the phenomenon of control-surface buzz

Stall Characteristics Obtained from Flight 10 of Northrop X-4 No. 2 Airplane (USAF No. 46-677)

Method for determining the frequency-response characteristics of an element or system from the system transient output response to a known input function

Analytical and experimental investigation of thrust augmentation of axial- and centrifugal-compressor turbojet engines by injection of water and alcohol in combustion chambers

Theoretical lift and damping in roll at supersonic speeds of thin sweptback tapered wings with streamwise tips, subsonic leading edges, and supersonic trailing edges

A comparison of theory and experiment for high-speed free-molecule flow

Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds : additional stability and control characteristics and the aerodynamic effects of external stores and ram jets

Wind-tunnel tests of a 0.16-scale model of the X-3 airplane at high subsonic speeds: stability and control characteristics

A numerical method for the stress analysis of stiffened-shell structures under nonuniform temperature distributions


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