Accession Number:

AD0852674

Title:

A Computer Analysis of Pressure Distribution over Slender Bodies at Subsonic Speeds.

Personal Author(s):

Corporate Author:

AIR FORCE INST OF TECH WRIGHT-PATTERSON AFB OH SCHOOL OF ENGINEERING

Report Date:

1969-03-01

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

Descriptive Note:

Master's thesis,

Pages:

0088

Descriptors:

Identifiers:

Subject Categories:

File Size:

0.00MB

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