Flow Field Visualization about External Axial Corners

By: Nasa, National Aeronautics and Space Adm

An experimental investigation was conducted to visualize the flow field about external axial corners. The investigation was initiated to provide answers to questions about the inviscid flow pattern for continuing numerical investigations. Symmetrical and asymmetrical corner models were tested at a Reynolds number per meter of 60,700,000. Oil-flow and vapor-screen photographs were taken for both models at angle of attack and yaw. The paper presents the results of the investigation in the form of oil-flow photographs and the surrounding shock wave location obtained from the vapor screens. Talcott, N. A., Jr. Langley Research Center NASA-TM-78682

• Format: Paperback
• Language: English
• ISBN: 1720155518
• ISBN13: 9781720155515
• Release Date: January 1
• Publisher: Independently Published
• Length: 26 Pages
• Weight: 0.19 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"