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Viewing:

AERO 201 Lectures 1-5

front 1

What are the four basic aerodynamic forces

back 1

Thrust, Lift, Drag, Weight

front 2

What is the equation of a unit vector

back 2

unit vector = vector / magnitude

front 3

what is the dot product of two vectors

back 3

|vector a| |vector b| cos (theta)

or (a1b1) + (a2b2) + (a3b3)

front 4

what is the cross product between two vectors

back 4

|vector a| |vector b| sin (theta)

front 5

What is Cramer's Rule

back 5

(practice problems)

front 6

What is sheer stress and tangential stress

back 6

tangential stress is when a force acts at an angle to the surface

Sheer stress is when a force acts parallel to the surface

Sheer stress is always tangential stress, but not all tangential stress is sheer stress

front 7

What are the four fundamental quantities of a fluid

back 7

Pressure, Density, Temperature, Velocity

front 8

A fluid is a substance which ______________________.

back 8

Cannot resist an applied sheer stress

front 9

What are the two types of fluids

back 9

Incompressible (liquid) and Compressible

front 10

Define Pressure

back 10

The normal force per unit area

P=F/A

Units: N/m^2, lb/ft^2

front 11

Define Density

back 11

Mass per unit volume

p=m/V

units: kg/m^3, slug/ft^3, lbm/ft^3

front 12

Define Temperature

back 12

average Kinetic Energy of the particles in a gas

KE=(3/2)kT where k is the Botlzmann constant (k=1.38 * 10^-23 J/K)

Units: K, C, R, F

front 13

when the flow is steady, the moving elements make fixed paths in space called ____________.

back 13

streamlines

front 14

What is a flow field?

back 14

(search this up later)

front 15

What is a perfect/ideal gas?

back 15

one which the intermolecular forces are negligible and where particles are widely separated (low density)

front 16

What is the equation of state?

back 16

P=pRT

R is the specific gas constant

front 17

What is specific volume?

back 17

The volume per unit mass. It is the inverse of density

front 18

What is this plane and what is it known for?

back 18

Convair B-58 Hustler

First supersonic strategic bomber capable of Mach 2 flight

Delta wing

front 19

what type of flow has a constant velocity that does not change or fluctuate with time?

back 19

A steady flow

front 20

What do you call the path taken by a moving fluid element

back 20

a streamline

front 21

What are the two aerodynamic forces?

back 21

Lift and Drag

front 22

The aerodynamic force exerted by the airflow on a surface stem from two sources:

back 22

1. Pressure Distribution on the surface

2. Shear stress (friction) distribution on the surface

front 23

What is shear stress?

back 23

the force per unit area acting tangentially (parallel) on a surface due to friction

tangential force times the surface area

front 24

What are the two types of payload?

back 24

Fixed payload (passengers, cargo, etc)

drop payload (skydivers, water, dust)

front 25

What happens when the pressure below the wing is greater than the pressure above the wing

back 25

Lift! The lift coefficient equation is C_L = L / q(bar) S where q(bar) is called the dynamic pressure, and it is given by q(bar) = (1/2)pv^2 (v is the free stream velocity)

front 26

Where does lift come from?

back 26

Lift occurs when a moving flow of fluid is turned by a solid object. The flow is turned in one direction and lift is generated in the opposite direction.

if there is no motion or no fluid, then there is no lift.

front 27

what is the difference between wind tunneling and actual flight?

back 27

Wind tunneling is when the headwinds are equal to the thrust, so the plane's speed relative to the ground is zero.

When the plane is moving relative to the ground, it is called actual flight

front 28

What are the three moves an airplane can make?

back 28

Pitch (up and down)

Roll (rolling around)

Yaw (left and right)

front 29

What is A?

back 29

Fuselage: Carries people, cargo, payload

front 30

What is G?

back 30

Vertical Stabilizer: yaw stability

front 31

What is F?

back 31

Rudder: provides yaw control (left and right motion)

front 32

What is E?

back 32

Horizontal Stabilizer: pitch stability (up and down)

H-stab, H tail

front 33

What is the combination of E, F and G called?

back 33

Empennage

front 34

What is D?

back 34

Main Landing Gear: supports aircraft weight on the ground (tricycle landing gear configuration)

front 35

What is c?

back 35

Nacelle: outer covering that encloses engine

front 36

What is B?

back 36

Nose Gear: Ground steering

front 37

What is H?

back 37

Wings: provide lift

front 38

What is I?

back 38

Aileron: provides roll control (left or right) (they are opposite of each other)

front 39

What is J?

back 39

Elevators: pitch control (up and down)

front 40

What is K?

back 40

Spoiler: Reduces lift and increases drag (independent movement of each other)

front 41

What is L?

back 41

Winglet: reduces drag (wing vortex control)

front 42

What is M?

back 42

Slat: aids in takeoffs and landings (increases or decreases wing surface area)

front 43

What is the longitudinal axis called and what causes the movement along it?

back 43

The roll axis: controlled by the yoke (turn the yoke left or right to turn the ailerons up and down)

Ailerons cause the movement by going up or down (located at the ends of the wings)

front 44

What is the lateral axis called and what causes the movement along it?

back 44

The pitch axis: controlled by pushing the yoke in to dive down and pulling them up to pitch up.

The elevators control the pitch by simultaneously flapping up or down

front 45

What is the vertical axis called and what causes the movement along it?

back 45

The yaw axis: causes the aircraft to spin left or right by pushing the right or left rudder pedal.

The rudder controls this movement by deflecting the airflow right or left from its position on the tail. Kind of like a shark tail.

front 46

What is the manufacturer, designation, and name of this aircraft?

back 46

The Consolidated B-24 Liberator

- world's most produced bomber (rapid production because of WW2)

- Called the flying coffin because there was only one exit, so the pilot couldn't escape

- straight (davis) wing, twin tail

front 47

what are airplanes with 1, 2 and 3 wings called?

back 47

Monoplane (Fairchild Republic A-10), Biplane (Boeing Stearman), triplane (Fokker Dr. I)

front 48

What is the name of this aircraft?

back 48

Fairchild Republic A-10 Thunderbolt

- AKA A-10 Warthog

-designed to provide close air support (CAS) to ground troops

-the only production-built aircraft designed solely for CAS

front 49

What is the name of this aircraft?

back 49

Boeing-Stearman Model 75

- military trainer aircraft

- after WW2, they were sold on the civilian market and were used for crop dusting, racing, and wing walking

front 50

What is the name of this aircraft?

back 50

Fokker Dr. I Red Baron

- WW1 fighter aircraft

front 51

What locations can the wings be placed in?

back 51

High wing (cessna 172), mid wing (f-16), low wing (Piper cherokee)

front 52

What is the name of this aircraft?

back 52

Cessna 172 Skyhawk

- more of these were built than any other aircraft

-most successful aircraft in history

front 53

What is the name of this aircraft?

back 53

General Dynamics (aka lockheed martin) F-16 Fighting Falcon

- world's most common fixed wing aircraft in the military

front 54

What is the name of this aircraft?

back 54

Piper Cherokee

- designed for flight training, taxi and personal use

- 4th most produced aircraft in history

front 55

What is the name of this aircraft?

back 55

Boeing 787 Dreamliner

- swept back wings

front 56

What are some other types of wings?

back 56

Swept back wings (boeing 787), swept forward wings (Grumman X-29A), canard at the front (Piaggio Avanti P180)

front 57

What is the name of this aircraft?

back 57

Northrop A-9A

-prototype that was passed up for the Fairchild A-10

front 58

What is the lift equation?

back 58

L = (1/2)pv^2SC_L

or

L = q(bar) S C_L

front 59

What is the dynamic pressure formula?

back 59

q(bar) = (1/2)pv^2

front 60

What are the atmospheric layers (starting from bottom to top) and how does this affect atmospheric conditions?

back 60

(troposphere, tropopause, stratosphere, stratopause, Mesosphere, mesopause, Thermosphere)

At the "spheres", temp changes linearly with altitude

at the "pauses", temp is constant

front 61

Hydrostatic equation

back 61

dP= -pgdhg

front 62

What is the geometric altitude

back 62

h_g, the geometric height above sea level is

front 63

what is the absolute altitude?

back 63

h_a the height measured from the center of the earth

front 64

What is the equation for the absolute altitude?

back 64

h_a = h_g +r (radius of the earth)