PRESSURE DISTRIBUTIONS AND OIL FILM PHOTOGRAPHS FOR MACH 5 FLOWS PAST FINS MOUNTED ON A FLAT PLATE. PART OF AN INVESTIGATION OF HYPERSONIC FLOW SEPARATION AND CONTROL CHARACTERISTICS,
Abstract
Pressure distributions and oil film photographs were obtained for Mach 5 flows past wedge shaped fins mounted on a sharp leading edge flat plate. Sharp and blunt leading edge fins of two different heights were tested for Reynolds numbers, based on the flat plate length, from 1.1 to 6.6 million. Data were obtained on both the fin and plate surfaces for model angles of attack between -5 and +10 degrees. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 01, 1963
- Accession Number
- AD0422031
Entities
People
- Louis G. Kaufman Ii.
Organizations
- Grumman