Accession Number : AD0852674
Title : A Computer Analysis of Pressure Distribution over Slender Bodies at Subsonic Speeds.
Descriptive Note : Master's thesis,
Corporate Author : AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING
Personal Author(s) : Tirres, Carlos
Report Date : MAR 1969
Pagination or Media Count : 88
Abstract : An analysis was made to determine validity of slender body theory in computing pressure distribution over slender conical bodies. Information is presented to correct for flow separation. Two methods were used to compute pressure distribution over conical bodies: source distribution with a cross-flow correction on a right circular cone; and complex potential method on elliptical cone. (Author)
Descriptors : (*REENTRY VEHICLES, SUBSONIC CHARACTERISTICS), PRESSURE, DISTRIBUTION, MATHEMATICAL ANALYSIS, FLOW SEPARATION, THESES, DATA PROCESSING, SLENDER BODIES, CONICAL BODIES.
Subject Categories : Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE