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- 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