Pressure Distributions on Three Bodies of Revolution to Determine the Effect of Reynolds Number up to and Including the Transonic Speed Range
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Swihart, John M↗
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An experimental study of water-pressure distributions during landings and planing of a heavily loaded rectangular flat-plate model
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Smiley, Robert F↗
Pressure Distributions at Mach Numbers from 0.6 to 1.9 Measured in Free Flight on a Parabolic Body of Revolution with Sharply Convergent Afterbody
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Stoney, William E , Jr↗
Low-speed Chordwise Pressure Distributions near the Midspan Station of the Slotted Flap and Aileron of a 1/4-scale Model of the Bell X-1 Airplane with a 4-percent-thick, Aspect-ratio-4, Unswept Wing
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Moseley, William C , Jr↗
An Investigation at High Subsonic Speeds of the Pressure Distributions on a 45 Degree Sweptback Vertical Tail in Sideslip with and Without a 45 Degree Sweptback Horizontal Tail Located on the Fuselage Center Line
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Wiley, Harleth G↗
Wind Pressure Distributions at Low Lift for the XF-92A Delta-wing Airplane at Transonic Speeds
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Keener, Earl R↗
Theoretical pressure distributions for some slender wing-body combinations at zero lift
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Byrd, Paul F↗
A Pressure-distribution Investigation of the Aerodynamic Characteristics of a Body of Revolution in the Vicinity of a Reflection Plane at Mach Numbers of 1.41 and 2.01
The changes in the aerodynamic characteristics of a body of revolution with a fineness ratio of 8 have been determined at Mach numbers of 1.41 and 2.01, a Reynolds number, based on body length, of 4.54 x 10 to the 6th power, and angles of incidence of 0 degrees and plus or minus 3 degrees as the position of the body is varied with respect to a reflection plane. The data are compared with theoretical results.
Gapcynski, John P↗
Investigation at High Subsonic Speeds of the Pressure Distributions on a 45 Degree Sweptback Horizontal Tail Mounted at 50-percent and 100-percent Vertical-tail Span
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Wiley, Harleth G↗
Flight-determined Pressure Distributions over a Section of the 35 Degree Swept Wing of the Douglas D-558-II Research Airplane at Mach Numbers up to 2
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Jordan, Gareth H↗
A low-speed investigation of a thin 60 degree delta wing equipped with a double slotted flap to determine the chordwise pressure distribution and the effect of vane size
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Croom, Delwin R↗
Preliminary Flight-determined Pressure Distributions over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers
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Jordan, Gareth H↗
Aerodynamic Characteristics and Pressure Distributions of a 6-percent-thick 49 Degree Sweptback Wing with Blowing over Half-span and Full-span Flaps
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Whittle, Edward F , Jr↗
Wing Pressure Distributions over the Lift Range of the Convair XF-92A Delta-wing Airplane at Subsonic and Transonic Speeds
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Keeener, Earl R↗
Hydrodynamic Pressure Distribution Obtained with a Streamline Body Equipped with Chine Strips
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Weinflash, Bernard↗
The Effect of Leading-edge Droop upon the Pressure Distribution and Aerodynamic Loading Characteristics of a 45 Degree Sweptback Wing at Transonic Speeds
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Schmeer, James W↗
Free-flight Tests to Determine the Power-on and Power-off Pressure Distribution and Drag of the NACA RM-10 Research Vehicle at Large Reynolds Numbers Between Mach Numbers 0.8 and 3.0
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Hoffman, Sherwood↗
Pressure Distribution and Aerodynamic Loadings for Several Flap-type Trailing-edge Controls on a Trapezoidal Wing at Mach Numbers of 1.61 and 2.01
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Lord, Douglas R↗