Accession Number : ADA334771
Title : Weapons Bay Turbulence Reduction Techniques
Corporate Author : AIR FORCE FLIGHT DYNAMICS LAB WRIGHT-PATTERSON AFB OH
Personal Author(s) : Clark, Rodney L.
PDF Url : ADA334771
Report Date : DEC 1975
Pagination or Media Count : 106
Abstract : This effort was directed toward experimental investigation of the static and dynamic pressure levels within shallow weapons bay cavities. Several turbulence reduction techniques and various bay geometry features were investigated. These included forward and aft blowing slots, fences positioned at the upstream cavity lip, and rounded cavity lips. Installation of a 50% porosity fence at the forward lip was determined to be the single most effective technique.
Descriptors : *TURBULENCE, *DYNAMIC PRESSURE, *STATIC TESTS, WEAPONS, FLIGHT TESTING, FORWARD AREAS, CAVITIES, REDUCTION, WIND TUNNEL TESTS, JET FIGHTERS, SLOTS, GEOMETRY, BAYS, SHALLOW DEPTH.
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE