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Fluid Mechanics  in  Aeronautics and Astronautics Fluid Mechanics  in  Aeronautics and Astronautics

Fluid Mechanics in Aeronautics and Astronautics - PowerPoint Presentation

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Fluid Mechanics in Aeronautics and Astronautics - PPT Presentation

Marc Williams School of Aeronautics and Astronautics Aeronautics Airplanes Astronautics Spacecraft Parts of Aero amp Astro Aerodynamics Design Dynamics amp Control Structures Propulsion ID: 702882

airplane air drag speed air airplane speed drag pushes flight throw direction energy mach sound thrust micro force boeing

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Slide1

Fluid Mechanics in Aeronautics and Astronautics

Marc WilliamsSchool of Aeronautics and AstronauticsSlide2

Aeronautics = AirplanesSlide3

Astronautics = SpacecraftSlide4

Parts of Aero & Astro

Aerodynamics

Design

Dynamics & Control

Structures

PropulsionSlide5
Slide6

Three forces from fluidsLIFT - Force perpendicular to flight direction

The Air pushes the airplane “up”DRAG - Force opposite the flight direction

The Air pushes the airplane “back”THRUST - Force in the flight directionInternal pressure inside the engine pushes the aircraft/rocket forwardSlide7

LIFT

Newton say : The air pushes the airplane up So

The airplane pushes the air downSlide8

Cessna Citation Slide9

Boeing 777Slide10

Boeing 757Slide11

DRAG

The air sticks to the airplane, pushing it back (Viscosity== Friction drag)

The airplane imparts kinetic energy to the air behind it…. This energy comes from the engines, And shows up as a drag

(Induced Drag, or Drag due to Lift)

Slide12

Flight Regimes – A Vocabulary

0

0 1.0 2.0 3.0 6.0

Mach Number – M

Altitude

(1000 ft.)

100

80

60

40

20

Subsonic

Supersonic

Hypersonic

Structural Limit

(Dynamic pressure and heating)

Aerodynamic

Limit

Transonic

V = flight speed

a = speed of sound

M = V / aSlide13

Wing Loading (N/m

2

)

All the Worlds Flyers

Flyers meeting MAV requirements abound in nature

Flyers with most remarkable performance leverage unsteady aerodynamics

Flapping provides access to game-changing aerodynamic mechanisms for meeting MAV requirements

Conventional Aircraft

(Steady)

Large Birds

(Quasi-steady)

Small Birds (Transition)

Insects/Hummingbirds

(Unsteady)

Cruising Speed (m/s)

Weight (N)Slide14

Micro Air Vehicles (MAVs)

Unmanned aerial systems becoming for missions too dull, dirty, dangerous, or difficult for pilotsPersistent ISRChemical/biological sensing

“Over the hill”/“Around the corner” scoutingOperation space is changingUrban canyonsBuilding interiors

Subterranean caverns/bunkers

MAVs are new class of vehicle to fill new operational roles

Images from wikipedia.org, defense-update.com, delta.tudelft.nlSlide15

DYNAMICS AND CONTROL

http://www.grc.nasa.gov/WWW/K-12/airplane/alr.htmlSlide16

Mach Number Effects

Mach Number = Speed / Speed of Sound Speed of Sound = 340 m/s = 770 mph

Mach squared = Kinetic Energy / Thermal EnergySlide17

An

F/A-18 Hornet at

transonic speed Slide18

F4 phantom ii breaking the sound barrier Slide19
Slide20

Mars Exploration Rover

(MER)

aeroshell, artistic renditionSlide21

Thrust

Thrust is produced by throwing something opposite to the direction you want to go (Newton again) You can throw air

You can throw hot exhaust gases You can throw rocks… but fluids are easier to work withSlide22

Air ThrowerSlide23

http://www.youtube.com/watch?v=nSQzvimD3cc

Turbofan Engine

This throws air and hot exhaust gasesSlide24

Turbofan FlowpathSlide25

Tomahawk Cruise MissileSlide26

Mi-24 Hind Military Aviation Helicopter

Air ThrowerSlide27

Joint Strike Fighter- Marine Version

Lift Fan

Another Air ThrowerSlide28

OSPREY- Tilt Rotor

And another… but you get to change the throw direction Slide29

Rockets – Pure Hot Gas ThrowersSlide30

How a Rocket Produces ThrustSlide31

ROCKETS

BIG (SSME)Slide32

A micro-thruster array measuring one-quarter the size of a penny,

designed by a TRW-led team for use on micro-,

nano- and pico-satellites, has successfully demonstrated its functionality in a live fire test aboard a

Scorpius

sub-orbital sounding rocket. Individual

micro-electromechanical system (MEMS) thrusters, each a poppy seed-sized

cell fueled with lead

styphnate

propellant, fired more than 20 times at 1-second

Intervals during the test staged at the White Sands Missile Range.

Each thruster delivered 10(-4) Newton seconds of impulse.

ROCKETS: SMALLSlide33

Sidewinder

Air to Air supersonic missileSlide34
Slide35

THE ENDHave a great summerSlide36
Slide37

Dynamic Stall on an AirfoilSlide38

Boeing 757Slide39

Vortex break-up on a delta wing at high incidence Slide40