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