Studies of von Karman's similarity theory and its extension to compressible flows : a similarity theory for turbulent boundary layer over a flat plate in compressible flow
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Lin, C C↗
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Studies of von Karman's similarity theory and its extension to compressible flow : investigation of turbulent boundary layer over a flat plate in compressible flow by the similarity theory
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Shen, S F↗
An Extension of the 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
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BODIES - SURFACE CONDITIONS↗
On the form of the turbulent skin-friction law and its extension to compressible flows
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Donaldson, Coleman Dup↗
Hovering Flight Tests of a Four-engine-transport Vertical Take-off Airplane Model Utilizing a Large Flap and Extensible Vanes for Redirecting the Propeller Slipstream
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Tosti, Louis P↗
Correlation, evaluation, and extension of linearized theories for tire motion and wheel shimmy
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Smiley, Robert F↗
Investigation of the effects of leading-edge chord-extensions and fences in combination with leading-edge flaps on the aerodynamic characteristics at Mach numbers from 0.40 to 0.93 of a 45 degree sweptback wing of aspect ratio 4
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Spreemann, Kenneth P↗
Effects of Horizontal-tail Position and a Wing Leading-edge Modification Consisting of a Full-span Flap and a Partial-span Chord-extension on the Aerodynamic Characteristics in Pitch at High Subsonic Speeds of a Model with a 45 Degree Sweptback Wing
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Morrison, William D , Jr↗
Transition-flight Investigation of a Four-engine-transport Vertical-take-off Airplane Model Utilizing a Large Flap and Extensible Vanes for Redirecting the Propeller Slipstream
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Tosti, Louis P↗
An Exploratory Investigation of the Relative Merits of Split and Chord-extension Flaps on a 45 Degrees Swept-back Wing
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Hopkins, Edward J↗
Pressure-distribution Measurements over an Extensible Leading-edge Flap on Two Wings Having Leading-edge Sweep of 42 Degrees and 52 Degrees
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Salmi, Reino J↗
Investigation of Extensible Wing-tip Ailerons on an Untapered Semispan Wing at 0 Degree and 45 Degrees Sweepback
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Hagerman, John R↗
Spin-tunnel Investigation of a Model of a 60 Degree Delta-wing Airplane to Determine the Spin, Recovery, and Longitudinal Trim Characteristics Throughout an Extensive Range of Mass Loadings
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Klinar, Walter J↗
Extension of boundary-layer heat-transfer theory to cooled turbine blades
An equation for average heat transfer of a surface was derived when the boundary layer changed from laminar to turbulent. Influences on the heat transfer through a laminar boundary layer of Mach number, temperature ratio (gas temperature divided by wall temperature), and exponents of gas-property temperature relations were shown to be relatively small for air with Mach numbers less than 2 and temperature ratios between 1 and 4. Good agreement was obtained with experimental results from cylinders, an airfoil, and turbine blades.
HEAT TRANSFER, AERODYNAMIC↗
Investigation of the effects of leading-edge chord-extensions on the aerodynamic and control characteristics of two sweptback wings at Mach numbers 1.41, 1.62, and 1.96
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Ellery, B May, Jr↗
Fundamental flame velocities of pure hydrocarbons III : extension of tube method of high flame velocities - acetylene-air mixtures
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Levine, Oscar↗
Effect of Leading-edge Chord-extensions on Subsonic and Transonic Aerodynamic Characteristics of Three Models Having 45 Degrees Sweptback Wings of Aspect Ratio 4
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Goodson, Kenneth W↗
Low-speed Static Longitudinal and Lateral Stability Characteristics of a Model with Leading-edge Chord-extensions Incorporated on a 40 Degree Sweptback Circular-arc Wing of Aspect Ratio 4 and Taper Ratio 0.50
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Goodson, Kenneth W↗