Accession Number : AD0450660


Title :   INVESTIGATION OF STING SUPPORT INTERFERENCE EFFECTS ON THE DYNAMIC AND STATIC STABILITY CHARACTERISTICS OF A 10-DEG CONE AT MACH NUMBERS 2.5, 3.0, AND 4.0,


Corporate Author : ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN


Personal Author(s) : Uselton, B L


Full Text : https://apps.dtic.mil/dtic/tr/fulltext/u2/450660.pdf


Report Date : Nov 1964


Pagination or Media Count : 22


Abstract : Tests were conducted in Tunnel D of the von Karman Gas Dynamics Facility to investigate sting support interference effects on the dynamic and static stability characteristics of a 10-deg half-angle cone. A free oscillation, cross-flexuje pivot balance system was used. Data were obtained at Mach numbers of 2.5, 3.0, and 4.0 at Reynolds numbers ranging from 0.45 x 10 to 6th power. Selected test results are presented, and comparisons are made with first and second- order potential flow theory and conical flow theory.


Descriptors :   *MOUNTING BRACKETS , AERODYNAMIC CHARACTERISTICS , CONICAL BODIES , INTERFERENCE , MODEL TESTS , NOSE CONES , STABILITY , SUPERSONIC CHARACTERISTICS , SUPERSONIC WIND TUNNELS , WIND TUNNEL MODELS


Subject Categories : Couplers, Fasteners, and Joints


Distribution Statement : APPROVED FOR PUBLIC RELEASE