Accession Number : AD0863276
Title : Air Defense Aerodynamic Design Investigation.
Descriptive Note : Final rept.,
Corporate Author : AUBURN UNIV AL ENGINEERING EXPERIMENT STATION
Personal Author(s) : Drummond, Alastair M.
Report Date : DEC 1969
Pagination or Media Count : 11
Abstract : An overview of the Interim Reports is presented as well as significant material from progress reports. The main areas of work lay in developing a proper aerodynamic simulation procedure and the use of this procedure in comparing winged and wingless configurations, as well as some specific configurations. (Author)
Descriptors : (*GUIDED MISSILES, AERODYNAMIC CHARACTERISTICS), AERODYNAMIC CONFIGURATIONS, WINGS, GUIDED MISSILE SIMULATORS, GUIDED MISSILE TRAJECTORIES, PERFORMANCE(ENGINEERING), OPTIMIZATION, ANGLE OF ATTACK.
Subject Categories : Guided Missiles
Distribution Statement : APPROVED FOR PUBLIC RELEASE