Skip to content

SEARCH · Search NASA

Results for “PRESSURE DISTRIBUTION - AIRFOILS - CASCADES”

Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.

SourceResearch connectionFrom yearThrough year

Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.

At least 469 records · Page 26

All sources NASA NTRS DOE OSTI

NASA NTRS1954

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

Explore the source record for details and available documents.

Moseley, William C , Jr↗

NASA NTRS1954

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

Explore the source record for details and available documents.

Wiley, Harleth G↗

NASA NTRS1954

Wind Pressure Distributions at Low Lift for the XF-92A Delta-wing Airplane at Transonic Speeds

Explore the source record for details and available documents.

Keener, Earl R↗

NASA NTRS1955

Theoretical pressure distributions for some slender wing-body combinations at zero lift

Explore the source record for details and available documents.

Byrd, Paul F↗

NASA NTRS1955

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↗

NASA NTRS1954

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

Explore the source record for details and available documents.

Wiley, Harleth G↗

NASA NTRS1955

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

Explore the source record for details and available documents.

Jordan, Gareth H↗

NASA NTRS1955

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

Explore the source record for details and available documents.

Croom, Delwin R↗

NASA NTRS1955

Preliminary Flight-determined Pressure Distributions over the Wing of the Douglas X-3 Research Airplane at Subsonic and Transonic Mach Numbers

Explore the source record for details and available documents.

Jordan, Gareth H↗

NASA NTRS1955

Aerodynamic Characteristics and Pressure Distributions of a 6-percent-thick 49 Degree Sweptback Wing with Blowing over Half-span and Full-span Flaps

Explore the source record for details and available documents.

Whittle, Edward F , Jr↗

NASA NTRS1955

Wing Pressure Distributions over the Lift Range of the Convair XF-92A Delta-wing Airplane at Subsonic and Transonic Speeds

Explore the source record for details and available documents.

Keeener, Earl R↗

NASA NTRS1955

Hydrodynamic Pressure Distribution Obtained with a Streamline Body Equipped with Chine Strips

Explore the source record for details and available documents.

Weinflash, Bernard↗

NASA NTRS1955

The Effect of Leading-edge Droop upon the Pressure Distribution and Aerodynamic Loading Characteristics of a 45 Degree Sweptback Wing at Transonic Speeds

Explore the source record for details and available documents.

Schmeer, James W↗

NASA NTRS1955

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

Explore the source record for details and available documents.

Hoffman, Sherwood↗

NASA NTRS1956

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

Explore the source record for details and available documents.

Lord, Douglas R↗

NASA NTRS1956

Force, Moment, and Pressure-distribution Characteristics of Rectangular Wings at High Angles of Attack and Supersonic Speeds

Explore the source record for details and available documents.

Pitts, William C↗

NASA NTRS1956

Force and Pressure-distribution Investigation to High Angles of Attack on All-movable Triangular and Rectangular Wings in Combination with a Body at Supersonic Speeds

Explore the source record for details and available documents.

Hill, William A↗

NASA NTRS1953

Correlation by the hypersonic similarity rule of the pressure distributions and wave drags for minimum-drag nose shapes at zero angle of attack

Explore the source record for details and available documents.

Jorgensen, Leland H↗