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