Experimental measurements of the wall static pressure on a yawed, tangent-ogive-cylinder model in supersonic flow are reported. The model tested was six calibers in length and had a one-caliber ogive section. Measurements were obtained at six longitudinal stations on the cylinder portion of the model for 15 deg increments in circumferential position at M = 2, 3, 4 and for angles of attack up to 10 deg. The data have been tabulated for convenience in evaluating inviscid flow field computations. These data should provide a good test for the coupling of subsonic, transonic, and supersonic inviscid flow computation techniques.
Measurements of wall static pressure on a yawed tangent-ogive-cylinder model
Messungen des statischen Wanddrucks an einem Spitzbogenzylindermodell bei Gierbewegungen
US Government Reports ; 1-50
1976
50 Seiten
Report
Englisch
NTRS | 1976
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