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BASIC AERODYNAMICS PART I

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Presentation on theme: "BASIC AERODYNAMICS PART I"— Presentation transcript:

1 BASIC AERODYNAMICS PART I
Federal Aviation Administration PRESENTED BY: Dennis H. Whitley FAASTeam Lead Representative NORTH FLORIDA REGION

2 MY MOTTO SHOW ME A PILOT THAT CAN’T ANSWER A CORRELATIVE QUESTION AND/OR CAN’T PERFORM A GIVEN TASK, & I’LL SHOW YOU A PILOT THAT DOESN’T UNDERSTAND WHAT HE/SHE IS TRYING TO ACCOMPLISH.

3 FLIGHT INSTRUCTING MUST NOT BE THE BY-PRODUCT OF BUILDING FLIGHT HOURS.

4 BUILDING FLIGHT HOURS MUST BE THE BY-PRODUCT OF FLIGHT INSTRUCTING.

5 SAFETY COMMITMENT VS DEDICATION

6 THIS DISCUSSION IS BASED ON SUBSONIC AIRCRAFT AND WILL BE
“VERY BASIC” “NO FORMULAS” “VERY LITTLE MATH”

7 4 FORCES LIFT/WEIGHT/THRUST/DRAG
WE WILL TALK ABOUT ATMOSPHERIC PRESSURE 4 FORCES LIFT/WEIGHT/THRUST/DRAG GROUND EFFECT TURNING TENDENCIES TRIM DEVICES AERODYNAMICS OF SPINS SLIPS/SKIDS ADVERSE YAW

8 WHAT IS ATMOSPHERIC PRESSURE?

9 ATMOSPHERIC PRESSURE IS THE WEIGHT OF ALL THE AIR UPON THE SURFACE OF THE EARTH.

10 HOW WAS ATMOSPHERIC PRESSURE MEASURED?
WHAT DOES 30 hg MEANS? HOW WAS ATMOSPHERIC PRESSURE MEASURED?

11 36 YARD STICK 36 INCHES TALL

12 36 YARD STICK

13 36 YARD STICK

14

15 HOW WAS THE DROP OF PRESSURE WITH ALTITUDE VERIFIED?

16

17 HOW WAS THE WEIGHT OF THE AIR DETERMINED?

18

19

20 A PRESSURE DIFFERENTIAL GAUGE
WHAT IS AN ALTIMETER? A PRESSURE DIFFERENTIAL GAUGE

21 HG 5 40 10 35 30 25 20 15 HG 5 40 10 35 30 25 20 15 FROM SOURCE FROM SOURCE HG 5 40 10 35 30 25 20 15

22 Kollsman Window Static Port

23 static port pressure 31.00 hg. sea level pressure 31.00 hg.

24 static port pressure 23.00 hg. sea level pressure 31.00 hg.

25 SEA LEVEL PRESSURE CORRECTED FOR NONSTANDARD TEMPERATURE.
WHAT IS ALTIMETER SETTING? SEA LEVEL PRESSURE CORRECTED FOR NONSTANDARD TEMPERATURE. 25

26 WHAT IS THE MAIN REASON THAT AN AIRPLANE IS ABLE TO FLY?
BECAUSE OF THE WEIGHT OF THE AIR. In other words the aerodynamic effect air has on the aircraft.

27 DEFINITION OF AERODYNAMICS
The branch of science that deals with the forces produced by air flowing over specially shaped surfaces called airfoils.

28 IS THERE ANY THING WRONG WITH THIS PICTURE? TWO THINGS
THE FLOWING OF THE RELATIVE WIND THE DIRECTION OF THE RELATIVE WIND

29 CAN WE FLY WITH A FLAT WING?

30 3RD LAW: For every action there is an equal and opposite reaction.
1ST LAW: Every object in a state of uniform motion tends to remain in that state of motion unless an external force is applied to it. 3RD LAW: For every action there is an equal and opposite reaction. AT CRUISE COSTANT ALTITUDE

31

32 MINIMUM MANEUVERING SPEED
SLOW FLIGHT

33 STALL PA-28 SERIES

34 WHAT IS THE DEFINITION OF FOIL? TO PREVENT FROM BEING SUCCESSFUL
TO THWART

35 AIRFOIL AN AIRFOIL IS AN AIR DEFLECTOR
Any surface designed to deflect the airflow passing over it or striking it, and thereby obtaining an useful reaction AN AIRFOIL IS AN AIR DEFLECTOR

36 HOW MANY AIRFOILS ARE THERE?

37 HORIZONTAL STABILIZER.
AIRPLANE WING. AILERONS. SLATS LANDING FLAPS. VERTICAL STABILIZER. RUDDER. HORIZONTAL STABILIZER. ELEVATOR/STABILATOR TRIM TABS. PROPELLER. ROTOR BLADE. FUSELAGE. FEARING. STRUTS.

38 WHAT IS LIFT?

39 A FORCE CREATED BY A DEFLECTION OF AIR
AND PRESSURE DIFFERENTIAL AROUND AN AIRFOIL. IS CALLED LIFT WHEN IT ACTS UPWARD. WHEN IT ACTS DOWNWARD IS CALLED NEGATIVE LIFT. WHEN IT ACTS SIDEWAYS IS CALLED SIDE LIFT. WHEN IT ACTS FORWARD IS CALLED THRUST

40 HOW IS LIFT CREATED? AIR PASSING BY AN AIRFOIL
DEFLECTION -- ISSAC NEWTON AIR’S CHANGE OF DIRECTION--BERNOULLI'S PRINCIPLE PRESSURE DIFERENTIAL-- BERNOULLI'S PRINCIPLE

41

42 WHAT’S WRONG WITH THIS PICTURE

43

44

45 CAN WE FLY WITHOUT THE HELP OF BERNOULLIS?

46

47

48 THRUST Thrust is a reaction force described quantitatively by Newton's second and third laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system.

49 Thrust is LIFT DIRECTED FORWARD.
LIFT is a reaction force described quantitatively by Newton's second and third laws. When a system expels or accelerates mass in one direction the accelerated mass will cause a proportional but opposite force on that system. Thrust is LIFT DIRECTED FORWARD.

50 THE PROPELLER’S DEFLECTION OF AIR

51

52

53 DRAG

54 PARASITE DRAG FORM INTERFERENCE

55 INDUCED DRAG GROUND EFFECT
COMMANDER TYSON

56 STAGNATION AREA UPWASH RELATIVE WIND DOWNWASH
ASSUMED LIFT ASSUMED ANGLE OF ATTACK DOWNWASH ASSUMED RELATIVE WIND IS THAT RIGHT?

57 STAGNATION AREA UPWASH RELATIVE CURRENT DOWNWASH

58 ASSUMED LIFT INDUCED ANGLE OF ATTACK INDUCED LIFT INDUCED RELATIVE WIND

59 DOWNWASH ASSUMED LIFT INDUCED ANGLE OF ATTACK INDUCED LIFT INDUCED RELATIVE WIND

60 DOWNWASH ASSUMED LIFT INDUCED ANGLE OF ATTACK WING TIP VORTICES INDUCED LIFT TOTAL ENDUCED DRAG INDUCED RELATIVE WIND

61 WING THREE-DIMENSIONAL FLOW
UPWASH MODIFIES RELATIVE WIND DOWNWASH PULLS BACK ON LIFT VECTOR WING TIP VORTICES PULLS LIFT VECTOR FURTHER BACK

62 DOWNWASH ASSUMED LIFT WING TIP VORTICES TOTAL ENDUCED DRAG INDUCED ANGLE OF ATTACK INDUCED LIFT INDUCED RELATIVE WIND

63 DOWNWASH ASSUMED LIFT INDUCED ANGLE OF ATTACK INDUCED LIFT INDUCED RELATIVE WIND

64 ASSUMED LIFT INDUCED ANGLE OF ATTACK LIFT INDUCED RELATIVE WIND

65 WASHOUT

66 WHAT DOES THE STABILATOR DO?

67 WHAT DOES THE ANTI-SERVO TAB DO?

68 STABILIZED UNACCELERATED CLIMB

69 IF DESCENDING IN A 60 ° BANK HOW MANY G ’S?

70 DYHEADRAL

71

72

73 ADVERSE YAW

74 OVERBANKING TENDENCIES

75 MANEUVERING SPEED VA

76 LOAD FACTOR


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