aircraft mechanics n.
Skip this Video
Loading SlideShow in 5 Seconds..
Aircraft Mechanics PowerPoint Presentation
Download Presentation
Aircraft Mechanics

Loading in 2 Seconds...

play fullscreen
1 / 19

Aircraft Mechanics - PowerPoint PPT Presentation

  • Uploaded on

Aircraft Mechanics. Alan Altschuler (Mr. A). Forces and Moments on Aircraft. Forces L ift Drag /Thrust Inertia Gravitational (weight) Linear and Rotational Momentum Ground Support Weight Speed-Up Catapult Slow-Down Arrestment Parachute (Drag-chute) Pressures (self-balancing) Cabin

I am the owner, or an agent authorized to act on behalf of the owner, of the copyrighted work described.
Download Presentation

Aircraft Mechanics

An Image/Link below is provided (as is) to download presentation

Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author.While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server.

- - - - - - - - - - - - - - - - - - - - - - - - - - E N D - - - - - - - - - - - - - - - - - - - - - - - - - -
Presentation Transcript
aircraft mechanics

Aircraft Mechanics

Alan Altschuler (Mr. A)

forces and moments on aircraft
Forces and Moments on Aircraft
  • Forces
    • Lift
    • Drag /Thrust
    • Inertia
      • Gravitational (weight)
      • Linear and Rotational Momentum
    • Ground
      • Support Weight
      • Speed-Up
        • Catapult
      • Slow-Down
        • Arrestment
        • Parachute (Drag-chute)
    • Pressures (self-balancing)
      • Cabin
      • Hydraulic and others (bleed air)
  • Moments
    • Pitch – Nose up and down
    • Roll – Left wing tip up with right down, and vice versa
    • Yaw – Nose left and right
axis systems on aircraft
Axis Systems on Aircraft
  • Local aircraft (x=aft, y=outboard (usually left), z=up – relative to aircraft (structure) – usually called Body Axes
    • Thrust is “mostly” negative local x
  • Air stream (x=streamwise flow (positive impinging on aircraft nose)
    • Wing angle of attack is “mostly” angle between local x and air stream x from pitch (also provided via roll velocity)
    • Vertical Tail angle of attack is “mostly” angle between local x airstream x from yaw (also provided via roll velocity)
    • Lift is positive airstream z
    • Drag is positive airstream x
  • Inertial (z=up relative to earth)
    • Weight is always inertial negative z
  • Direction Cosines
    • A method to rotate vectors among axis systems

Ground Configuration

All axis-systems aligned



Air Configuration

All axis-systems mis-aligned here






with earth

Aligned with airframe

Aligned with airflow




lift curve
Lift curve
  • Bernoulli
  • Angle of attack
  • Camber
  • Bernoulli
  • NACA airfoil
roll yaw coupling
Roll – Yaw Coupling
  • Due to asymmetry in the aircraft y-z and x-y planes
  • Can have roll-pitch and yaw-pitch coupling, but symmetry about aircraft x-z centerplane would make these couplings zero.
  • Interesting cases of asymmetry
    • Single-engine aircraft
    • Multi-engine aircraft without counter-rotating engines
      • E-2 tail (Hawkeye)
    • Single main-rotor helicopters
    • A-10 nose wheel (Warthog/Thunderbolt)
    • 2-bladed props

Principle axes

  • Linear
  • Angular
    • Issue with Most Helicopters
    • Banking a bicycle
    • Car
      • Tilting on an unbanked roadway
      • Roadway banking
  • Center of Gravity
newton s second law
Newton’s Second Law
  • F = ma ?
    • Not really
  • Actually, force equals the change in momentum over time
  • Momentum P = mv
  • In calculus F = dP/dt = d/dt (mv)

= m dv/dt + v dm/dt

  • In non-calculus F = DP/Dt = m Dv/Dt + v Dm/Dt
  • Dv/Dt = a
  • F = ma + v Dm/Dt
    • the second part is the “rocket” part, exhausted gas quickly from the body
lifting surfaces
Lifting Surfaces
  • Wing
    • Bi-plane wing structures
    • Winglet
  • Horizontal Stabilizer (Tail)
  • Vertical Stabilizer (Tail)
  • Canard
    • X-29
  • Fuselage
    • F-14 body lift

Ground Configuration - parked

Air Configuration – steady level flight

control surfaces
Control Surfaces
  • Elevators
  • Ailerons
  • Rudders
  • Pictures
  • Spoilers
  • Used less often
    • Speed brakes
    • Elevons (Space Shuttle)
    • “Flying” Horizontal Stabilizers (F-14)
      • Aka stabilators
landing gear alighting gear
Landing Gear(Alighting Gear)
  • Main Gear
    • Metering Pins
  • Nose Gear
  • Tail Gear (DC3)
  • Parachute/Drag Chute (Space Shuttle)
  • Tail Hook (Navy)
  • Tow Bar (Navy)
  • Emergencies
    • USAF – Tail Hook
    • USN – Barricade1
    • USN – Barricade2
level turn
Level Turn
  • Increased g’s are need to maintain altitude AND turn simultaneously
coordinated turn
Coordinated Turn
  • 1-g in the body axis-z direction is generated for passenger comfort.
  • Combined rolling, pulling up when banked, and turning produced a “coordinated turn”.
  • The aircraft actually accelerates down in the inertial-z axis and loses altitude
aero elastics






  • Static
    • Lift
    • Roll
    • Pitch
    • Divergence
  • Dynamic
    • Flutter
    • Example1
    • Example2
    • Non-aero effect
      • Shimmie
  • Unswept wings (whose chordlines align with the airstream) do not have a negative increment of angle of attack (gliders)
  • Swept wings provide greater area with less frontal area (less drag)
  • a & b are chord-lines
  • perpendicular to elastic axis,
  • b deflects up more than a,
  • producing an elastic
  • increment of negative
  • angle of attack in the airstream



Outbd tip

deflects up



sonic effects
Sonic Effects
  • Sub-sonic
    • Center of pressure at approx 25% chord
  • Super-sonic
    • Center of pressure at approx 40% chord
    • Wing sweep (F-14)

Pressure distribution

ground effects
Ground Effects

Case Study

  • US Navy wanted to perform a test of the E-2C Landing Gear at the Maximum Sink Speed
    • Sink speed is the vertical component of the landing velocity.
  • This is no fun for the pilot, whose back can be injured.
  • It is very difficult to do due to ground effects.
  • In real life the Navy is concerned with aircraft carrier combined pitch, roll and vertical deck motions when the aircraft lands.
clean upper wing air passage
“Clean” Upper Wing Air Passage

Case Study

  • Often airframe structural analysts are asked to review issues regarding parts manufactured out-of-tolerance.
  • These parts may be scrapped, reworked or used as-is. Sometimes new parts are added, often called “doublers”
  • Aerodynamicists rarely permit violation of the upper cover’s Outer Mole Line (OML), the shape of the wing on the top, but care little about the lower cover’s OML.
  • Typically, no doublers are allowed on the upper cover.