Accession Number:

AD0265987

Title:

THE FLOW OF TWO ADJACENT PLANE SUPERSONIC JETS PAST FLAT PLATE WINGS, IV. CALCULATIONS WITH SUBSONIC LEADING EDGES ON THE STARBOARD SIDE

Descriptive Note:

Corporate Author:

CALIFORNIA UNIV BERKELEY INST OF ENGINEERING RESEARCH

Personal Author(s):

• HOLT,M.
• LEE,S.C.

Report Date:

1961-10-01

Pagination or Media Count:

1.0

Abstract:

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

Descriptors:

• *PRESSURE
• *SUBSONIC FLOW
• *SUPERSONIC FLOW
• COMPLEX VARIABLES
• DELTA WINGS
• ELECTRONIC SCANNERS
• EXPERIMENTAL DATA
• NUMERICAL INTEGRATION
• JET AIRCRAFT
• MATHEMATICAL ANALYSIS
• TABLES(DATA)
• TRANSFORMATIONS(MATHEMATICS)

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE