Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
14045 results returnedSearch results
- Recovery and time-response characteristics of six thermocouple probes in subsonic and supersonic flow
- Calculation of the supersonic pressure distribution on a single-curved tapered wing in regions not influenced by the root or tip
- Extrapolation techniques applied to matrix methods in neutron diffusion problems
- Theoretical analysis of incompressible flow through a radial-inlet centrifugal impeller at various weight flows II : solution in leading-edge region by relaxation methods
- Gust-tunnel investigation of the effect of a sharp-edge gust on the flapwise blade bending moments of a model helicopter rotor
- Tensile properties of 7075-T6 and 2024-T3 aluminum-alloy sheet heated at uniform temperature rates under constant load
- Circumferential distribution of propeller-slipstream total-pressure rise at one radial station of a twin-engine transport airplane
- An experimental investigation of regions of separated laminar flow
- Theoretical analysis of incompressible flow through a radial-inlet centrifugal impeller at various weight flows 1: solution by a matrix method and comparison with an approximate method
- An Analysis of the Stability and Ultimate Compressive Strength of Short Sheet-Stringer Panels with Special Reference to the Influence of Riveted Connection Between Sheet and Stringer
- A limited investigation of the effect of three vortex-generator configuration on the effectiveness of a plain flap on an unswept wing
- Flow studies on flat-plate delta wings at supersonic speed
- On slender delta wings with leading-edge separation
- A study of boundary-layer transition and surface temperature distributions at Mach 3.12
- The effectiveness of wing vortex generators in improving the maneuvering characteristics of a swept wing airplane at transonic speeds
- 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