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旋翼机飞行手册 ROTORCRAFT FLYING HANDBOOK

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Comments regarding this handbook should be sent to U.S. Department of Transportation, Federal Aviation Administration, Airman Testing Standards Branch, AFS-630, P.O. Box 25082, Oklahoma City, OK 73125.
AC 00-2, Advisory Circular Checklist, transmits the current status of FAA advisory circulars and other flight information publications. This checklist is free of charge and may be obtained by sending a request to U.S. Department of Transportation, Subsequent Distribution Office, SVC-121.23, Ardmore East Business Center, 3341 Q 75th Avenue, Landover, MD 20785.
AC00-2 also is available on the Internet at http://www.faa.gov/abc/ac-chklst/actoc.htm. 

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CONTENTS
 

HELICOPTER Chapter 1—Introduction to the Helicopter
The Main Rotor System ..........................................1-1
Fully Articulated Rotor System ..........................1-1
Semirigid Rotor System......................................1-2
Rigid Rotor System ............................................1-2
Antitorque Systems .................................................1-2
Tail Rotor ............................................................1-2
Fenestron.............................................................1-2
NOTAR®............................................................1-2
Landing Gear...........................................................1-2
Powerplant...............................................................1-3
Flight Controls.........................................................1-3

Chapter 2—General Aerodynamics
Airfoil ......................................................................2-1
Relative Wind .....................................................2-2
Blade Pitch Angle ...............................................2-2
Angle of Attack...................................................2-2
Lift ...........................................................................2-3
Magnus Effect.....................................................2-3
Bernoulli’s Principle ...........................................2-3
Newton’s Third Law of Motion..........................2-4
Weight......................................................................2-4
Thrust.......................................................................2-5
Drag .........................................................................2-5
Profile Drag ........................................................2-5
Induced Drag ......................................................2-5
Parasite Drag.......................................................2-6
Total Drag ...........................................................2-6

Chapter 3—Aerodynamics of Flight
Powered Flight ........................................................3-1
Hovering Flight .......................................................3-1

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