Search
Search U.S. government technical reports digitized or harvested by TRAIL.
Keyword Search
4176 results returnedSearch results
- Compression Shocks of Detached Flow
- The Distribution of Loads on Rivets Connecting a Plate to a Beam Under Transverse Loads
- Drag Reduction by Suction of the Boundary Layer Separated Behind Shock Wave Formation at High Mach Numbers
- Force and Pressure-Distribution Measurements on a Rectangular Wing With a Slotted Droop Nose and With Either Plain and Split Flaps in Combination or a Slotted Flap
- Investigations on Reductions of Friction on Wings, in Particular by Means of Boundary Layer Suction
- NACA Conference on Aerodynamic Problems of Transonic Airplane Design
- A Method for Estimating Heat Requirements for Ice Prevention Gas Heated Hollow Propeller Blades
- Introduction to the Problem of Rocket-Powered Aircraft Performance
- Wind-tunnel investigation of the effect of tab balance on tab and control-surface characteristics
- The Performance of a Composite Engine Consisting of a Reciprocating Spark-Ignition Engine, a Blow-Down Turbine, and a Steady-Flow Turbine
- Experimental Studies of Knock-Limited Blending Characteristics of Aviation Fuels 3 - Aromatics and Cycloparaffins
- Laboratory Investigation of Ice Formation and Elimination in the Induction System of a Large Twin-Engine Cargo Aircraft
- Wind-Tunnel Investigation of Effects of Unsymmetrical Horizontal-Tail Arrangements on Power-on Static Longitudinal Stability of a Single-Engine Airplane Model
- Theoretical Lift Distribution and Upwash Velocities for Thin Wings at Supersonic Speeds
- Review of an Investigation of Ceramic Coatings for Metallic Turbine Parts and Other High-Temperature Applications
- A Method of Calculating the Compressive Strength of Z-Stiffened Panels That Develop Local Instability
- Effect of Exhaust Pressure on the Cooling Characteristics of an Air-Cooled Engine
- Analysis, Verification, and Application of Equations and Procedures for Design of Exhaust-Pipe Shrouds
- Analytical and Experimental Investigation of Bolted Joints
- The Calculation of the Heat Required for Wing Thermal Ice Prevention in Specified Icing Conditions
- Generalized Performance Comparison of Large Conventional, Tail Boom, and Tailless Airplanes
- A Method for Estimating Heat Requirements for Ice Prevention on Gas-Heated Hollow Propeller Blades
- High-Speed Wind-Tunnel Tests of an NACA 0009-64 Airfoil Having a 33.4-Percent-Chord Flap With an Overhang 20.1 Percent of the Flap Chord
- A Further Investigation of the Meteorological Conditions Conducive to Aircraft Icing
- Investigation of the pressure-loss characteristics of a turbojet inlet screen
- Diagonal tension in curved webs
- Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners panels of various stiffener spacings that fail by local buckling
- Determination of plate compressive strengths
- Theoretical supersonic wave drag of untapered sweptback and rectangular wings at zero lift
- Charts for stress analysis of reinforced circular cylinders under lateral loads
- Investigation of NACA 65(sub 112) A111 (approx.) airfoil with 0.35-chord slotted flap at Reynolds numbers up to 25 million
- Investigation of the Aileron and tab of a spring-tab lateral-control system in the Langley 19-foot pressure tunnel
- Hydrodynamic impact loads in smooth water for a prismatic float having an angle of dead rise of 30 degrees
- Experimental and calculated characteristics of three wings of NACA 64-210 and 65-210 airfoil sections with and without 2 degree washout
- Effect of variation in diameter and pitch of rivets on compressive strength of panels with Z-section stiffeners: Panels of various lengths with close stiffener spacing
- The stability derivatives of low-aspect-ratio triangular wings at subsonic and supersonic speeds
- Stress analysis by recurrence formula of reinforced circular cylinders under lateral loads
- Pressure-distribution measurements on the rotating blades of a single-stage axial-flow compressor
- Low-speed static stability and damping-in-roll characteristics of some swept and unswept low-aspect-ratio wings
- Method for calculating wing characteristics by lifting-line theory using nonlinear section lift data
- Wake measurements behind a wing section of a fighter airplane in fast dives
- Two-dimensional wind-tunnel investigation of four types of high-lift flap on an NACA 65-210 airfoil section
- Wind-Tunnel Investigation of the Effect of Power and Flaps on the Static Longitudinal Stability Characteristics of a Single-Engine Low-Wing Airplane Model
- Preliminary Investigation of a Gas Turbine With Sillimanite Ceramic Rotor Blades
- Propeller-Loudness Charts for Light Airplanes
- Some Considerations on an Airfoil in an Oscillating Stream
- Variation of Hydrodynamic Impact Loads With Flight-Path Angle for a Prismatic Float at 0 and -3 Degree Trim and With a 22 1/2 Degree Angle of Dead Rise
- Wing Pressure-Distribution Measurements Up to 0.866 Mach Number in Flight on a Jet-Propelled Airplane
- The Langley Two-Dimensional Low-Turbulence Pressure Tunnel
- The Effect of Compressibility on the Growth of the Laminar Boundary Layer on Low-Drag Wings and Bodies