Last updated on May 8th, 2020 at 12:09 am
Aircraft Aerodynamics and Rigging
Aircraft Aerodynamics, Structures and Systems (3811 Questions)
Category B2 – Aircraft Aerodynamics Exams ( 128 questions 180 min),
Aircraft Structures
easa_part_66_academy ch02
Chapter 01: Aircraft Structures (70 pages),
Chapter 02: Aerodynamics, Aircraft Assembly, and Rigging (70 pages),
Chapter 03: Aircraft Fabric Covering ( 24 pages),
Chapter 04: Aircraft Metal Structural Repair ( 114pages),
Chapter 05: Aircraft Welding ( 38 pages),
Chapter 06: Aircraft Wood and Structural Repair ( 28 pages),
Chapter 07: Advanced Composite Material ( 58 pages),
Chapter 08: Aircraft Painting and Finishing ( 22 pages),
Chapter 09: Aircraft Electrical System ( 106 pages),
Chapter 10: Aircraft Instrument Systems (86pages),
Chapter 11: Communication and Navigation (78 pages),
Chapter 12: Hydraulic and Pneumatic Power Systems (54 pages),
Chapter 13: Aircraft Landing Gear Systems (96 pages),
Chapter 14: Aircraft Fuel System (62 pages),
Chapter 15: Ice and Rain Protection (32 pages),
Chapter 16: Cabin Environmental Control Systems (62 pages),
Chapter 17: Fire Protection Systems (22 pages),
Aircraft Structures
Three topics that are directly related to the manufacture, operation, and repair of aircraft are: Aerodynamics , and rigging. Aircraft Aerodynamics, and Rigging Each of these subject areas, though studied separately, Aircraft Aerodynamics Aircraft Assembly, and Rigging eventually connect to provide a scientific and physical understanding of how an aircraft is prepared for flight.
Aircraft Assembly
A logical place to start with these three topics is the study of basic aerodynamics. By studying aerodynamics, a person becomes familiar with Aircraft Aerodynamics, Aircraft Assembly, and Rigging the fundamentals of aircraft flight.
As an airplane travels through the air, the air particles close the airplane are upset and move around the airplane. The air particles are pushed aside a lot of like a vessel makes a bow wave as it travels through the water. On the off chance that the airplane goes at a low speed, ordinarily under 250 mph, the thickness of the air
stays steady. In any case, at higher paces, a portion of the vitality of the airplane goes into packing the air and locally evolving the thickness of the air. The greater and heavier the airplane, the more air it dislodges and the more noteworthy impact pressure has on the airplane Aircraft Assembly.
This impact turns out to be progressively significant as speed increments. Close
also, past the speed of sound, around 760 mph (adrift level), sharp aggravations produce a shockwave that influences both the lift and drag of an airplane and stream conditions downstream of the shockwave. The shockwave structures a cone of pressurized air particles which move outward and rearward on the whole
headings and stretch out to the ground. The sharp arrival of the pressure, after the development by the shockwave, is heard as the sonic blast Aircraft Assembly.
Extra specialized data relating to fast optimal design can be found at book shops, libraries, and various sources on the Internet. As the plan of airplane advances and the velocities of airplane keep on expanding into the hypersonic go, new materials and drive frameworks should be created. This is the test for engineers, physicists, and originators of airplane later on.
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