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Пікірлер: 45
@karaebdi83374 жыл бұрын
Flaps can help thanks for coming back
@jean-davidlegrand35684 жыл бұрын
Please more videos like this...
@sotoleeis3 жыл бұрын
something as simple as waxing your aircraft regularly. (it will decrease parasite drag) it may allow your aircraft to fly even up to 3 knots faster.
@DirkHav Жыл бұрын
I always wondered, is that really so much ?
@AarushKumar-wn4tl3 ай бұрын
@@DirkHav damn
@erich93011 ай бұрын
The two big factors that affect the speed at which the critical angle of attack is exceeded are weight (obviously) and G forces. Higher weight or G forces increase the stall speed, and lower weight or G forces decrease the stall speed. High-lift devices and other aerodynamic features may also come into play, but this is the most basic physics you can apply even to a paper airplane.
@Echo_Lima Жыл бұрын
vortex generators can reduce Vs and increase critical α
Power and flaps Power by increasing the thrust thus lift, and flaps by tilting the nose more downward but the airplane will stall in less aoa.
@LiangYuChen-sn6lyАй бұрын
Whoop whoop PULL UP Whoop whoop TERAIN TO LOW 1:20
@prateetdosi12164 жыл бұрын
Using Vortex Generator with Morphing
@DirkHav Жыл бұрын
What is Morphing ?
@solemnly983318 күн бұрын
CG position?
@streakurt3 ай бұрын
Can someone answer me, if (as defination) aoa is angle between relative wind and wing's cord then how airspeed change AoA while you don't change angle of your wings as physcially ?
@Onlyonemash7 ай бұрын
How about if we extend the trim tabs as that would push the aileron downwards and put the airplane to a straight level flight.
@darrelmiller26093 жыл бұрын
That depends on a lot of factors with weight being one of them. The heavier the aircraft the greater the AOA or The airspeed needs to be. Remember this though.... when ever the AOA is increased there is a portion of the weight vector shifted closer towards the drag vector.
@Northstar_0044 жыл бұрын
flaps and slats
@sheldonmcpherson270010 ай бұрын
Critical angle of attack can be at any airspeed why is the stall speed the IAS at the time the CAOA was met
@CJBuggs7 ай бұрын
Low aspect wings and tapered wings
@sharoz63004 жыл бұрын
Flaps will reduce stall speed
@alexs.p.r43572 жыл бұрын
but they increase the aoa
@user-cy7oz8vm4h Жыл бұрын
@@alexs.p.r4357they don’t increase the AOA, the increase lift by extending the camber of the wing but thr reduce the critical AOA
@adlzz27117 ай бұрын
@@alexs.p.r4357they increase the stall angle
@vatsalpatel64014 ай бұрын
They increase camber ( surface area )@@alexs.p.r4357
@AarushKumar-wn4tl3 ай бұрын
@@user-cy7oz8vm4h The AOA increases because the effective chord line, which runs from the leading edge of the wing to the trailing edge of the flap, pivots up
@davidgerlach11324 ай бұрын
Smaller wing load could reduce stall speed?
@zarmril Жыл бұрын
I have a question. Saying that "flaps decreases stall speed" may not be true? A certain amount of flaps can increase lift, at the expense of drag. However, in this case, the ratio between lift generated and induced drag is so that more lift is generated than drag is created. But if flaps were extended to a point in which induced drag was greater than lift generation, wouldn't stall speed thereby be increased since more lift is required to maintain an altitude? Ah, I just answered my own question. In a C172, stall recovery procedure is to have flaps no greater than let's say 20 degrees. This is because greater than 20 degrees generates more drag than lift, which can cause a secondary stall if you are not able to trade altitude for airspeed. Right?
@youpeppe124 Жыл бұрын
U have no lift without incrementing drag. So the flaps do increase lift at any configuration but because of drag it's not convenient to use them until you are landing and you actually need that drag to slow down and to increase also the Vz (descent). In fact if you use more than 10° flaps for Takeoff you will have more lift for sure and reduce the ground roll, but as soon as you lift off the drag will cause you not to climb as easily as you do without flaps. In a go-around one of the things you do is infact retract flaps once the speed is appropriate because as flaps retract stall speed increases. Hope that helps
@erich93011 ай бұрын
The opposition force to drag is thrust, not lift. Not enough *thrust* is the reason you bring the flaps up for a stall recovery.
@clayton41154 ай бұрын
Reduce the aoa will reduce stall speed
@tionormanw5 ай бұрын
It depends on what is your intention. With the maksimum takeoff weight you want to increase lift and gain higher altitude and reduce the stall speed; you just need to set your Flaps for takeoff setting and put your speed on Vy or Vx. Or, reduce your weight.❤
@juanvolvoturbo3 жыл бұрын
A higher Coefficient of lift.
@comradecamarada67254 жыл бұрын
Wing Fences
@ianknappy2 жыл бұрын
Flight at less than 1g can reduce stall speed
@csaw70642 жыл бұрын
formation of ice
@donlsamuel4 жыл бұрын
Landing Gear in Down Position and Less weight in the plane
@fletcherharris57654 жыл бұрын
Flaps
@DirkHav2 жыл бұрын
Excess trust.
@ArcherAC3 Жыл бұрын
I'd answer less weight
@loutsont2985 Жыл бұрын
Not at once as clear to me as your other topics. Not always sure weather 'stall speed' is 'actual-', 'inevitable/laws of physics-' or 'wanted by pilot-' stall speed.
@erich93011 ай бұрын
I believe the term "stall speed" on its own is a little misleading. It implies that speed has something to do with a stall, which really it does not. I would say this video is "inevitable/laws of physics."