Accession Number : AD0095898

Title :   APPLICATION OF BOUNDARY LAYER CONTROL TO HELICOPTER ROTOR BLADES

Descriptive Note : Final rept. 29 Feb 56,

Corporate Author : CESSNA AIRCRAFT CO WICHITA KS

Personal Author(s) : HINTON, S.H. ; LODGE, D.W.

Report Date : 29 FEB 1956

Pagination or Media Count : 10

Descriptors :   *AIRFOILS, *BOUNDARY LAYER CONTROL, *BOUNDARY LAYER CONTROL, *GAS FLOW, *HELICOPTER ROTORS, *HELICOPTERS, *ROTOR BLADES (ROTARY WINGS), *SUCTION SLOTS, AERODYNAMIC CHARACTERISTICS, BOUNDARY LAYER, DESIGN, EFFECTIVENESS, EXHAUST SYSTEMS, FATIGUE (MECHANICS), INSTRUMENTATION, MATHEMATICAL ANALYSIS, OSCILLATION, STRESSES, TESTS.

Subject Categories : Helicopters
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE