Browse TRAIL Inventories

Velocity Distribution on Wing Sections of Arbitrary Shape in Compressible Potential Flow 3: Circulatory Flows Obeying the Simplified Density-Speed Relation

Variation With Temperature of Surface Tension of Lubricating Oils

A Study of Water Pressure Distribution During Landings with Special Reference to a Prismatic Model Having a Heavy Beam Loading and a 30 Degree Angle of Dead Rise

Stress-Strain and Elongation Graphs for Alclad Aluminum-Alloy 24S-T86 Sheet

The Effect of End Plates on Swept Wings at Low Speed

A Comparison of the Lateral Controllability with Flap and Plug Ailerons on a Sweptback-Wing Model

Development and Preliminary Investigation of a Method of Obtaining Hypersonic Aerodynamic Data by Firing Models Through Highly Cooled Gases

Free-Flight-Tunnel Investigation of Dynamic Longitudinal Stability as Influenced by the Static Stability Measured in Wind-Tunnel Force Tests Under Conditions of Constant Thrust and Constant Power

Sonic-Flow-Orifice Temperature Probe for High-Gas-Temperature Measurements

Calculated Engine Performance and Airplane Range for Variety of Turbine-Propeller Engines

Measurements of Section Characteristics of a 45 Degree Swept Wing Spanning a Rectangular Low-Speed Wind Tunnel as Affected by the Tunnel Walls

Compressibility Correction for Turning Angles of Axial-Flow Inlet Guide Vanes

Pressure Distribution and Damping in Steady Pitch at Supersonic Mach Numbers of Flat Swept-Back Wings Having All Edges Subsonic

Effect of Heat-Capacity Lag on a Variety of Turbine-Nozzle Flow Processes

Foaming of Mixtures of Pure Hydrocarbons

Theoretical Analysis of Oscillations in Hovering of Helicopter Blades With Inclined and Offset Flapping and Lagging Hinge Axes

Pressure Distribution and Damping in Steady Roll at Supersonic Mach Numbers of Flat Swept-Back Wing with Subsonic Edges

Effects of an Aging Treatment on Life of Small Cast Vitallium Gas-Turbine Blades

Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 3: Methods for Determining Power and Efficiency

Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 1: Methods for Determining Heat-Transfer Characteristics

Preliminary Analysis of Problem of Determining Experimental Performance of Air-Cooled Turbine 2: Methods for Determining Cooling-Air-Flow Characteristics

Downwash in Vortex Region Behind Rectangular Half-Wing at Mach Number 1.91

Static Directional Stability of a Tandem-Helicopter Fuselage

Performance of 4600-Pound-Thrust Centrifugal-Flow-Type Turbojet Engine With Water-Alcohol Injection at Inlet

Dynamic Investigation of Turbine-Propeller Engine Under Altitude Conditions

Chordwise and Spanwise Loadings Measured at a Large Triangular Wing Having an Aspect Ratio of 2 and a Thin, Subsonic-Type Airfoil Section

Investigation at High Subsonic Speeds of Methods of Alleviating the Adverse Interference at the Root of a Swept-Back Wing

Analysis of Multiengine Transport Airplane Fire Records

Penetration of Liquid Jets into a High-Velocity Air Stream

Effects of the Lateral Oscillation of Fixing the Rudder and Reflexing the Flaps on the Bell X-1 Airplane

Exploratory Investigation of the Effect of Skewed Plain Nose Flaps on the Low-Speed Characteristics of a Large-Scale Triangular-Wing-Fuselage Model

Low-Speed Static Stability Characteristics of a Canard Model with a 45 Degree Sweptback Wing and a 60 Degree Triangular Horizontal Control Surface

Effect of an End Plate on the Aerodynamic Characteristics of a 20.55 Degree Sweptback Wing with an Aspect Ratio of 2.67 and a Taper Ratio of 0.5.: Transonic-Bump Method

Determination of Minimum Moments of Inertia of Arbitrarily Shaped Areas, Such as Hollow Turbine Blades

Lateral-Control Investigation at a Reynolds Number of 5,300,000 of a Wing of Aspect Ratio 5.8 Sweptforward 32 Degrees at the Leading Edge

High-Speed Aerodynamic Characteristics of a Lateral-Control Model 2: Modified NACA 0012-64 Section with a 26.6-Percent-Chord, Plain, Trailing-Edge Aileron; Wing Unswept and Swept Back 45 Degrees

Calculated Performance of Nuclear Turbojet Powered Airplane at Flight Mach Number of 0.9

A Design Study of Leading-Edge Inlets for Unswept Wings

Pressure Coefficients at Mach Numbers from 0.60 to 0.85 for a Semispan Wing with NACA 0012-64 Section, 20-Percent-Chord Plain Aileron, and 0 Degree and 45 Degree Sweepback

Effect of Retractable Ignition Plug on Plug Fouling by Carbon Deposits

Investigation at a Mach Number of 1.93 to Determine Lift, Drag, Pitching-Moment, and Average Downwash Characteristics for Several Missile Configurations Having Rectangular Wings and Tails of Various Spans

Further Investigation of a Gas Turbine with National Bureau of Standards Body 4811C Ceramic Rotor Blades

Altitude-Chamber Performance of British Roll-Royce Nene II Engine 4: Effect of Operational Variables on Temperature Distribution at Combustion-Chamber Outlets

A Lift-Cancellation Technique in Linearized Supersonic-Wing Theory

On the Theory of the Propagation of Detonation in Gaseous Systems

On the Particular Integrals of the Prandtl-Busemann Iteration Equations for the Flow of a Compressible Fluid

Laws of Flow in Rough Pipes

Investigation of the NACA 3-(3)(05)-05 Eight-Blade Dual-Rotating Propeller at Forward Mach Numbers to 0.925

Investigation of the NACA 4-(4)(06)-057-45a and NACA 4-(4)(06)-57-45b Two-Blade Swept Propellers at Forward Mach Numbers to 0.925

Flight Measurements of Base Pressure on Bodies of Revolution With and Without Simulated Rocket Chambers


Published Year

Subject

Author

‹‹ previous 1 2 ... 147 148 149 150 151 152 153 ... 280 281 next ››