Accession Number : AD0053510


Title :   AN ANALYSIS OF THE EFFECTS OF BOUNDARY-LAYER-CONTROL AND PROPELLER CONFIGURATION ON THE PERFORMANCE OF AN ASW TYPE AIRPLANE


Corporate Author : WICHITA STATE UNIV KS


Personal Author(s) : RAZAK, KENNETH


Report Date : AUG 1954


Pagination or Media Count : 1


Descriptors :   *AIRPLANES, AERODYNAMIC CHARACTERISTICS, ANTISUBMARINE WARFARE, BOUNDARY LAYER CONTROL, CONFIGURATION, DRAG, LIFT, OPERATION, PROPELLER BLADES.


Distribution Statement : APPROVED FOR PUBLIC RELEASE