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THE FLOW OF TWO ADJACENT PLANE SUPERSONIC JETS PAST FLAT PLATE WINGS, IV. CALCULATIONS WITH SUBSONIC LEADING EDGES ON THE STARBOARD SIDE
CALIFORNIA UNIV BERKELEY INST OF ENGINEERING RESEARCH
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Using the general formulae derived earlier Quart. J. Mech. Appl. Math. IV 4419-431, 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
APPROVED FOR PUBLIC RELEASE