Accession Number : AD0736456
Title : Wind Tunnel Investigation of the Transonic Aerodynamic Characteristics of a Full-Scale Flight Path Accelerometer (Follow-On Test).
Descriptive Note : Final rept.,
Corporate Author : ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AIR FORCE STATION TENN
Personal Author(s) : Shadow,T. O.
Report Date : FEB 1972
Pagination or Media Count : 41
Abstract : A wind tunnel investigation was conducted on a full-scale flight path accelerometer (FPA), to eliminate shock interaction effects between the angle-of-attack and sideslip vanes and to determine angle-of-attack and angle-of-sideslip vane position errors. The shock interference effects were controlled by increasing the axial separation distance between the angle-of-attack and sideslip vanes.
Descriptors : (*ACCELEROMETERS, TRANSONIC CHARACTERISTICS), ANGLE OF ATTACK, ERRORS, WIND TUNNEL MODELS, MODEL TESTS, AERODYNAMIC CONFIGURATIONS
Subject Categories : Test Facilities, Equipment and Methods
Distribution Statement : APPROVED FOR PUBLIC RELEASE