THE FLOW OF TWO ADJACENT PLANE SUPERSONIC JETS PAST FLAT PLATE WINGS, IV. CALCULATIONS WITH SUBSONIC LEADING EDGES ON THE STARBOARD SIDE
Abstract
Using the general formulae derived earlier (Quart. J. Mech. Appl. Math. IV; 4:419-431, 51) further surface pressure distributions are calculated on delta wings placed in two adjacent uniform supersonic jets. Five cases are considered wh the port et lea ing edge lies outside and the starboard leading edge lies inside the respective Mach semi-cones. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 01, 1961
- Accession Number
- AD0265987
Entities
People
- M. Holt
- S.c. Lee
Organizations
- University of California, Berkeley