Aerodynamics exam 3 Flashcards

0
Q

When does pitch control airspeed?

A

When power is not available

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1
Q

Design phases (3)

Essay

A

—Conceptual phase (where to place power plant, landing gear, etc)

—Preliminary design (configuration)

—Detail design (supporting structure)

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2
Q

List problems when landing in heavy rain

Essay

A

1) rain momentum is down and back
2) rain film on aircraft increases weight
3) rain film is roughed by falling rain drops causing a decrease in aerodynamic Efficiency
4) rain drops hit the aircraft in an uneven pattern causing pitching and rolling

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3
Q

List problems when reaching force divergence Mach #

Essay

A

1) increase CD
2) decrease in CL
3) change in pitching moment as CP (center of pressure) changes

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4
Q

Benefits of swept wing in supersonic flight

Essay

A

1) raises Mach crit
2) reduces amount of CD increase
3) wing is within Mach cone

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5
Q

Sir George cailey

A

Concept of rigid wing

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6
Q

Which wing design has the least induced drag?

A

Elliptical

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7
Q

Why are balloons aero static vehicles?

A

Because they rise in still air

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8
Q

Aircraft certified under part 25?

A

Military Aircraft are not certified under part 25

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9
Q

Parts included in parasite drag

Essay

A
  • leakage
  • form
  • adverse flow
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10
Q

Adverse flow?

A

Adverse pressure gradient

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11
Q

How does load factor affect stall speed?

A

Square root of load factor x stall speed = new stall speed

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12
Q

Most common prop on modern complex aircraft?

A

Constant speed

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13
Q

Formula TOD (pressurized)

A

3 times altitude
6 times groundspeed

Unpressurized—-
No more than 500FPM

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14
Q

SHP

A

On turbine aircraft

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15
Q

1.2 Mach is in what range?

A

Transonic range

16
Q

Optimum fineness ratio

A

3

17
Q

Problems encountered in transonic flight

Essay

A

1) force divergence
2) wave drag
- boundary layer separation changes aerodynamic force
- drag increases dramatically due to wave drag
- loss of lift
- shock induced stall
- tuck under
- buffet
- control surface buzz
- control effectiveness
Holy crap