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.


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/a334771.pdf


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