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2. Stall (fluid dynamics) - Wikipedia

   en.wikipedia.org/wiki/Stall_(fluid_dynamics)

   V S: Stall speed: the speed at which the airplane exhibits those qualities accepted as defining the stall. [26]: 8 V S0: The stall speed or minimum steady flight speed in landing configuration. [27] The zero-thrust stall speed at the most extended landing flap setting. [26]: 8 V S1: The stall speed or minimum steady flight speed obtained in a ...

3. Coffin corner (aerodynamics) - Wikipedia

   en.wikipedia.org/wiki/Coffin_corner_(aerodynamics)

   The minimum such speed is the stall speed, or V SO. The indicated airspeed at which a fixed-wing aircraft stalls varies with the weight of the aircraft but does not vary significantly with altitude. At speeds close to the stall speed the aircraft's wings are at a high angle of attack. At higher altitudes, the air density is lower than at sea level.

4. V speeds - Wikipedia

   en.wikipedia.org/wiki/V_speeds

   Stall speed or minimum steady flight speed for which the aircraft is still controllable. [7] [8] [9] V S 0: Stall speed or minimum flight speed in landing configuration. [7] [8] [9] V S 1: Stall speed or minimum steady flight speed for which the aircraft is still controllable in a specific configuration. [7] [8] V S R: Reference stall speed. [7 ...

5. Speeding in a California school zone? Here’s what ‘when ...

   www.aol.com/speeding-california-school-zone...

   “If it’s 10 a.m. and children are corralled in a fenced area during recess, then motorist may go (the regular speed limit if it’s) safe to do so,” Olsen wrote.

6. Wing loading - Wikipedia

   en.wikipedia.org/wiki/Wing_loading

   The Monarch Butterfly has a very low 0.168 kg/m 2 wing loading The McDonnell Douglas MD-11 has a high 837 kg/m 2 maximum wing loading. In aerodynamics, wing loading is the total weight of an aircraft or flying animal divided by the area of its wing.

7. Maneuvering speed - Wikipedia

   en.wikipedia.org/wiki/Maneuvering_speed

   V A is the design maneuvering speed and is a calibrated airspeed.Maneuvering speed cannot be slower than and need not be greater than V c. [4]If is chosen by the manufacturer to be exactly the aircraft will stall in a nose-up pitching maneuver before the structure is subjected to its limiting aerodynamic load.