Browse TRAIL Inventories

Wind-Tunnel Measurements of the Dynamic Cross Derivative (Rolling Moment Due to Yawing Velocity and to Acceleration in Sideslip) of the Douglas D-558-II Airplane and Its Components at Supersonic Speeds Including Description of the Technique

Tests of Aerodynamically Heated Multiweb Wing Structures in a Free Jet at Mach Number 2: Two Aluminum-Alloy Models of 20-Inch Chord With 0.064- and 0.081-Inch-Thick Skin

The Effect of Base Bleed on the Base Pressure, Lift, Drag, and Pitching Moment of a 10-Percent-Thick Blunt-Base Airfoil at a Mach Number of 2.72

Effects of Some Leading-Edge Modifications, Section and Plan-Form Variations, and Vertical Position on Low-Lift Wing Drag at Transonic and Supersonic Speeds

Effects of Taper Ratio on the Longitudinal Characteristics at Mach Numbers From 0.6 to 1.4 of a Wing-Body-Tail Combination Having an Unswept Wing of Aspect Ratio 3

Effects of a Detached Tab on the Hinge-Moment and Effectiveness Characteristics of an Unswept Trailing-Edge Control on a 60 Degree Delta Wing at Mach Numbers From 0.75 to 1.96

Effect of Inlet Temperature on Rotating Stall and Blade Vibrations in a Multistage Axial-Flow Compressor

Effect of Reduced Stator-Blade Trailing-Edge Thickness on Over-All Performance of a Transonic Turbine

Effect of Several Modifications to Center Body and Cowling on Supercritical Performance of a Supersonic Inlet at Mach Number of 2.02

Effects of Boundary-Layer Separation on Normal Force and Center of Pressure of a Cone-Cylinder Model With a Large Base Flare at Mach Numbers From 3.00 to 6.28

Effects of Combining Auxiliary Bleed With Ejector Pumping on the Power Requirements and Test-Section Flow of an 8-Inch by 8-Inch Slotted Tunnel

Experimental Flutter Results for Cantilever-Wing Models at Mach Numbers Up to 3.0

Drag Investigation of a Swept-Wing Fighter-Airplane Model Incorporating Two Drag-Rise-Reducing Fuselage Revisions

A Drop Test for the Evaluation of the Impact Strength of Cermets

A Dynamic-Model Study of the Effect of Added Weights and Other Structural Variations on the Blade Bending Strains of an Experimental Two-Blade Jet-Driven Helicopter in Hovering and Forward Flight

Effect of an All-Movable Wing-Tip Control on the Longitudinal Stability of 60 Degree Sweptback-Wing-Indented-Body Configuration Equipped With Fences at Transonic Speeds

High-Altitude Performance of an Experimental Turbojet Combustor Having Variable Primary-Air Admission

Aircraft-Fuel-Tank Design for Liquid Hydrogen

Correlation of Vibratory Root Failures and Stress Distribution in J65 Compressor Blades

A Correlation of Two-Dimensional Data on Lift Coefficient Available With Blowing-, Suction-, Slotted-, and Plain-Flap High-Lift Devices

Axial-Flow Compressor Rotating-Stall and Rotor-Blade Vibration Survey

Aerodynamic Characteristics of a 1/4-Scale Model of the Duct System for the General Electric P-1 Nuclear Powerplant for Aircraft

Acceleration Characteristics of a Turbojet Engine With Variable-Position Inlet Guide Vanes

Aerodynamic Loading Characteristics in Sideslip of a 45 Degree Sweptback Wing With and Without a Fence at High Subsonic Speeds

An Investigation of Drains Discharging Liquid Into Subsonic and Transonic Streams

An Investigation of Jet Effects on Adjacent Surfaces

Investigation of Interference Lift, Drag, and Pitching Moment of a Series of Triangular-Wing and Body Combinations at a Mach Number of 1.94

An Investigation of Loads on Ailerons at Transonic Speeds

An Investigation of the Effects of Rapid Skin Heating on Box Beams Loaded in Bending

A Flight Investigation at Transonic Speeds of a Model Having a Triangular Wing of Aspect Ratio 4

Flight Measurements at Transonic Speeds of the Buffeting Characteristics of the XF-92A Delta-Wing Research Airplane

Flight Investigation of the Supersonic Area Rule for a Straight Wing-Body Configuration at Mach Numbers Between 0.8 and 1.5

Flight Investigation of the Effect of Underwing Propulsive Jets on the Lift, Drag, and Longitudinal Stability of a Delta-Wing Configuration at Mach Numbers From 1.23 to 1.62

Flight Investigation of a Roll-Stabilized Ram-Jet Test Vehicle Over a Mach Number Range of 2.3 to 2.7

Flight Investigation at Supersonic Mach Numbers of an Automatic Acceleration Control Missile in Which Rate Damping Is Obtained From a Linear Accelerometer Placed Ahead of the Missile Center of Gravity

High-Speed Cascade Tests of a Blade Section Designed for Typical Hub Conditions of High-Flow Transonic Rotors

The Hydrodynamic Force Characteristics of Streamline Bodies of Revolution Having Fineness Ratios of 6, 9, and 12 With and Without Chine Strips

Low-Speed Wind-Tunnel Investigation of a Triangular Sweptback Air Inlet in the Root of a 45 Degree Sweptback Wing

An Investigation of the Aerodynamic Characteristics of Thin Delta Wings With a Symmetrical Double-Wedge Section at a Mach Number of 6.9

Investigation of Equilibrium Temperatures and Average Laminar Heat-Transfer Coefficients for the Front Half of Swept Circular Cylinders at a Mach Number of 6.9

Investigation of the Lateral Stability Characteristics of the Douglas X-3 Configuration at Mach Numbers From 0.6 to 1.1 by Means of a Rocket-Propelled Model

Lateral Stability Characteristics at Low Lift Between Mach Numbers of 0.85 and 1.15 of a Rocket-Propelled Model of a Supersonic Airplane Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degrees Sweepback

Experimental Evaluation of Boron-Hydrocarbon Slurry in a 16-Inch Ram-Jet Combustor

Flow and Force Characteristics of 2-Percent-Thick Airfoils at Transonic Speeds

Initial Experiments on the Aerodynamic Cooling Associated With Large-Scale Vortical Motions in Supersonic Flow

Flight Measurements of the Transonic Drag of Models of Several Isolated External Stores and Nacelles

Flight Tests of a Delta-Wing Vertically Rising Airplane Model Powered by a Ducted Fan

Force and Pressure Measurements on Several Canopy-Fuselage Configurations at Transonic Mach Numbers 1.41 and 2.01

Flutter Experiences With Thin Pointed-Tip Wings During Flight Tests of Rocket-Propelled Models at Mach Numbers From 0.8 to 1.95

Investigation at Transonic Speeds of Aerodynamic Characteristics of a Semicircular Air Inlet in the Root of a 45 Degree Sweptback Wing


Published Year

Subject

Author

‹‹ previous 1 2 ... 91 92 93 94 95 96 97 ... 143 144 next ››