PROPOSED INVESTIGATION OF VISCOUS-INVISCID EFFECTS IN HYPERSONIC FLOW IN THE AEDC GAS DYNAMICS FACILITY TUNNEL B. PHASE II
Abstract
A test program is presented for a series of hypersonic research tests to provide detailed data for pressure distribution and heat transfer over several model configurations. The model configurations include delta planforms 70 degrees lambda 0 degrees dihedral, 70 degrees lambda 10 degrees cathedal, 70 degrees lambda 10 degrees dihedral, 60 degrees lambda 0 degrees dihedral, 75 degrees lambda 0 degrees dihedral, fin-flat plate interference (90 degrees Fin), and 45 degrees fin-flat plate interference.
Document Details
- Document Type
- Technical Report
- Publication Date
- Mar 28, 1960
- Accession Number
- AD0256172