Wing Root Airfoil Naca

CURTISS ELECTRIC PROPELLER TYPE(3 BLADES) C-5320-A20 BLADE NO 109354-12

BLADE Ol AMETER 130 CONTROL NO. ANO 10010 LOW PITCH SETTING 18 5# HIGH PITCH SETTING 535* PROPELLER CUFFS CONSTANT SPEED TYPE

FUEL TANK CAPACITIES TWO RELEASEABLE FUEL TANKS 58 GALLONS EACH FUSELAGE FUELTANK 117 GALLONS (SELF-SEALING TYPE) RELEASEABLE FUEL TANKS ARE ATTACHED TO THE LOWER SURFACE OF THE STUB WINGS A RELEASING CONTROL IS LOC ATEO BELOW THE RIGHT AND LEFT HAND SHELVES OF THE PILOT'S COCKPIT THE TANKS ARE MADE OF ALUMINUM ALLOY.

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  • addolorata marcelo
    How to draw a airfoil in aircraft engineering drawing .ppt?
    8 years ago

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