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
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE