Measurements of Wall Static Pressure on a Yawed Tangent-Ogive-Cylinder Model.
Abstract
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Nov 01, 1976
- Accession Number
- ADA033275
Entities
People
- John J. Reba
- Walter B. Sturek
Organizations
- Ballistic Research Laboratory