Applied Mechanics 1966
DOI: 10.1007/978-3-662-29364-5_108
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Experimentelle Untersuchungen laminarer Grenzschichten bei instabiler Schichtung

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Cited by 5 publications
(2 citation statements)
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“…It is evident from Figs. 6a and b that the substitution in equation (16) of the more realistic value for y of 1.33 for otherwise the same conditions has negligible effect on the distributions of M, U and Re x along the pressure surface. Figs.…”
Section: Laminar1sation Condition As a Design Criterion For Turbine Bmentioning
confidence: 93%
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“…It is evident from Figs. 6a and b that the substitution in equation (16) of the more realistic value for y of 1.33 for otherwise the same conditions has negligible effect on the distributions of M, U and Re x along the pressure surface. Figs.…”
Section: Laminar1sation Condition As a Design Criterion For Turbine Bmentioning
confidence: 93%
“…to 36 for U'.,/11 0, of 0.003. Subsequent investigations, including those of Tani (15), Wortmann (16,17), T'ani and Aihara (18) and Winoto, Durao and Crane (19), have been essentially concerned with visualization of, and velocity measurements in, the laminar boundary layer to identify the system of vortices on concave surfaces, and their effects on transition. Tani and Aihara (18) concluded that these were indirect in modifying the development of Tollmien-Schlichting waves by inducing a spanwise variation of boundary-layer thickness.…”
Section: Measurements Over Concave Surfacesmentioning
confidence: 99%