Static Pressure

35 books
Calibration of seven-hole pressure probes for use in fluid flows with large angularityGregory G. Zilliac

Calibration of seven-hole pressure probes for use in fluid flows with large angularity

Gregory G. Zilliac

1990No page data
Theoretical derivation and calibration technique of a hemispherical-tipped, five-hole probeScott O. Kjelgaard
⏱ 24m

Theoretical derivation and calibration technique of a hemispherical-tipped, five-hole probe

Scott O. Kjelgaard

198824 pp.
Statics of soil mediaVasiliǐ Vasil'evich Sokolovskiǐ
⏱ 3h 57m

Statics of soil media

Vasiliǐ Vasil'evich Sokolovskiǐ

1960237 pp.
Calibration of seven-hole pressure probes for use in fluid flows with large angularityGregory G. Zilliac

Calibration of seven-hole pressure probes for use in fluid flows with large angularity

Gregory G. Zilliac

1990No page data
Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnelElizabeth B. Plentovich
⏱ 21m

Orifice-induced pressure error studies in Langley 7- by 10-foot high-speed tunnel

Elizabeth B. Plentovich

198621 pp.
Experimental cavity pressure measurements at subsonic and transonic speedsElizabeth B. Plentovich
⏱ 1h 13m

Experimental cavity pressure measurements at subsonic and transonic speeds

Elizabeth B. Plentovich

199373 pp.
Static presssure position error calibration of the NAE T-33 C-FSKHJ. F. Aitken
⏱ 33m

Static presssure position error calibration of the NAE T-33 C-FSKH

J. F. Aitken

198733 pp.
Graphic and Analytic Statics in Theory and Comparison: Their Practical Application to the ...Robert Hudson Graham
⏱ 6h 14m

Graphic and Analytic Statics in Theory and Comparison: Their Practical Application to the ...

Robert Hudson Graham

1883374 pp.
A directionally insensitive static pressure probe for meteorological field useRichard W. Miksad
⏱ 19m

A directionally insensitive static pressure probe for meteorological field use

Richard W. Miksad

197519 pp.
Der brückenbauMichael Strukel

Der brückenbau

Michael Strukel

1900No page data
Static-pressure error of an airspeed installation on an airplane in high-speed dives and pull-outsLangley Aeronautical Laboratory
⏱ 16m

Static-pressure error of an airspeed installation on an airplane in high-speed dives and pull-outs

Langley Aeronautical Laboratory

194616 pp.
Evaluation of F/A-18A HARV inlet flow analysis with flight dataUnknown Author

Evaluation of F/A-18A HARV inlet flow analysis with flight data

Unknown Author

1995No page data
Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnelRichard J. Re

Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel

Richard J. Re

1998No page data
PSP measurement of stator vane surface pressures in a high speed fanJan Lepicovsky

PSP measurement of stator vane surface pressures in a high speed fan

Jan Lepicovsky

1998No page data
Flow through a rectangular-to-semiannular diffusing transition ductUnknown Author

Flow through a rectangular-to-semiannular diffusing transition duct

Unknown Author

1997No page data
Analysis of fluctuating static pressure measurements in the National Transonic FacilityWilliam B. Igoe
⏱ 3h 0m

Analysis of fluctuating static pressure measurements in the National Transonic Facility

William B. Igoe

1996180 pp.
Method for determining the time delay of the pitot-static tubing system of aircraftJ. H. Breeman
⏱ 16m

Method for determining the time delay of the pitot-static tubing system of aircraft

J. H. Breeman

198316 pp.
Rocket-based combined cycle engine technology developmentJ. R. DeBonis

Rocket-based combined cycle engine technology development

J. R. DeBonis

1996No page data
Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics TunnelD. M. Schuster

Aerodynamic measurements on a large splitter plate for the Langley Transonic Dynamics Tunnel

D. M. Schuster

2001No page data
The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbersElizabeth B. Plentovich

The application to airfoils of a technique for reducing orifice-induced pressure error at high Reynolds numbers

Elizabeth B. Plentovich

1986No page data
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