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Theoretical and experimental investigations of wall adaptation control in wind tunnel and hybrid wind tunnel testing

โœ Scribed by Th. Hottner


Publisher
Springer
Year
1995
Tongue
English
Weight
650 KB
Volume
19
Category
Article
ISSN
0723-4864

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โœฆ Synopsis


The hybrid wind tunnel principle is an economical alternative to classical wind tunnels. Wall adaptation tests are reported which are performed in a small scale arrangement duplicating original kinematic relations. A new method for controlling the quality of wall adaptation is presented which is based on the pressure distribution at the rigid wall. This procedure may also be applied for wall adaptation in conventional wind tunnel technique.

List of symbols cp pressure coefficient ( = (p--po~)lq~ ~ --2ulu~)

d diameter h height of test section k constant for cross flow pressure drop through perforated wall 1 length Ma Mach number p pressure q dynamicpressure(=2PMa2 ) r radius s gap width t time u, v disturbance velocity w flow velocity x coordinate in flow direction fl Prandtl factor boundary layer thickness ~c ratio of specific heats ~b adaptation coefficient-c~ (C~)r (subcritical flow)


๐Ÿ“œ SIMILAR VOLUMES


An experimental comparison of two adapta
โœ G. P. Russo; G. Zuppardi; M. Basciani ๐Ÿ“‚ Article ๐Ÿ“… 1995 ๐Ÿ› Springer ๐ŸŒ English โš– 564 KB

In the present work an experimental comparison is made between two adaptation strategies: the Iudd's method and the Everhart's method. A NACA 0012 airfoil has been tested at Mach numbers up to 0.4: models with chords up to 200 mm have been tested in a 200 mm x 200 mm test section. The two strategies