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George Geo
  • Member for 2 years, 11 months
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5 votes
Accepted

What is the Angle of Attack of this Propeller?

5 votes

Why would an F-35 take off with air brakes behind the cockpit extended?

2 votes

Why are there two red lines on the G-meter in the MiG-29?

1 vote

Why do jet nozzles close at different rates?

0 votes

Does it make sense to say an aircraft has an attitude of 3° or that it has a flight position of 3°?

0 votes

Is airflow deflected inwards or outwards by wing sweep?

0 votes

Does the F-4 Phantom use (have) differential horizontal tail deflection?

0 votes

How was flutter mitigated in jets such as the F-15 and F-16?

0 votes

What is the axis of rotation in a high alpha roll?

0 votes

Are canards actually more efficient?

0 votes

Under what circumstances does the F-16 and possibly similar fighters deploy leading edge slats?

0 votes

Why do jet engine fan blades have a twisted shape?

0 votes

Does slipstream on a single engine aircraft create a slight difference in wing strut loads during TO and Climb Out?

-1 votes

Is the movement of the leading edge flaps not symmetrical on the MiG-29?

-1 votes

Forces in a slipping turn

-1 votes

How does maximum speed vary with altitude?

-1 votes

What is the influence of yaw on P-factor?

-1 votes

What is the influence of yaw on P-factor?

-1 votes

What are the advantages and disadvantages of the MiG-29's horizontal stabilizers (not what do they do)?

-1 votes

Does the F-16 have a speed limiter?

-2 votes

What is a 'deep stall' and how can pilots recover from it?

-2 votes

What is the difference between the flight control systems of different F-16 models?

-2 votes

In a flat spin, does the F-16 use its rudder deflection against the rotation for recovering?

-2 votes

How does forward sweep of a wing affect the formation of shock waves?

-2 votes

Why does airflow separate from the wing during stall?

-2 votes

Why do Leading Edge Flaps (LEFs) create lift while down at slow speeds, but decrease lift while down at higher speeds?

-4 votes

What is the maximum angle the F-16 can turn in $x$ seconds while flying at corner speed?