2 edition of Measurement of skin friction at low subsonic speeds by the razor-blade technique found in the catalog.
Measurement of skin friction at low subsonic speeds by the razor-blade technique
Lionel Fitzroy East
Bibliography: p. 13.
|Statement||by L. F. East.|
|Series||Aeronautical Research Council. Reports and memoranda,, no. 3525, Reports and memoranda (Aeronautical Research Council (Grear Britain)) ;, no. 3525.|
|LC Classifications||TL526.G7 A4 no. 3525|
|The Physical Object|
|Number of Pages||24|
|LC Control Number||68069217|
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Speeds of Skin Friction at Low Subsonic by the Razor-Blade Technique By L. East, Ph.D. Reports and Memoranda No. * August, Summary.
The technique consists of forming a surface pitot-tube by placing a small segment of razor blade on. Measurement of skin friction at low subsonic speeds by This paper studies the measurement of wall shear stress vector fields in supersonic flows with shock waves using the shear-sensitive.
The Measurement Supersonic Flow by Film of Skin Friction in means of Heated Thin Gauges By B. Bellhouse and D. Schultz Reports and Memoranda No. * October, Summary. The application of heated thin film gauges to the measurement of. Download Citation | Addition of a Stanton Gauge to the Boundary Layer Data System | The Stanton gauge technique provides an indirect method for measurement of skin.
The material contained in this monograph has been divided into six main sections, in accordance with the specific applications of the pitot tube and other allied pressure probes, viz.
for impact pressure, static pressure, dynamic pressure, flow direction and vector velocity, skin friction as well as flow by: Full text of "Flow control [electronic resource]: fundamentals and practices" See other formats. This banner text can have markup.
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Aerospace Sci. ,Vol. 16, No. 2, pp. PergamonPress. Printedin Great Britain. PRESSURE P R O B E S F O R F L U I D MEASUREMENT S. H. C H U E Universiti Sains Malaysia* Summary--The material contained in this monograph has been divided into six main sections, in accordance with the specific applications of the pitot tube and other allied pressure probes, viz.