# Tag Info

91

The Gossamer Albatross is a human-powered plane with a top speed of 29 km/h (18mph). It was used to cross the English Channel and seems to meet the criteria of the question.

83

Because wings work on air moving past them, not ground moving below them. Heck, in a 35 knot headwind, the Antonov-2 could be rolling backwards at 2 knots and still take off!

65

I'd like to answer this question by debunking the premise of the question: that most plane crashes happen when planes fall out of the sky, and that it's like rock climbing where the higher you are, the more likely a fall will kill you. While it sounds believable, it's almost entirely false, and since it isn't diving out of the sky that kills you, lowering ...

61

The Antonov AN-2 has no stall speed quoted in the operating manual and can fly under full control at about 30 mph. Thus if the headwind is sufficiently large the aircraft will move backwards with respect to the ground.

61

It would likely create a more deadly situation. In aviation altitude is your friend. Generally speaking altitude in the case of an emergency buys you time to work the problem. Generally you want to be as high as practical for the aircraft in question. Altitude also buys you glide distance to find a suitable landing location in an emergency. Airplanes ...

59

This is because what you are looking at is the IAS indicator (Indicated Air Speed). This represents the amount of relative air which flows over and under the wings of the plane. This is what creates lift and enables the plane to fly. This is why this instrument is so important and belongs to the primary flight instruments. This is not to be confused with GS ...

52

The speed indicator in the cockpit shows indicated airspeed. Indicated airspeed is usually different than GPS speed, due to wind and aerodynamic effects. GPS speed is your speed with respect to the ground. If you are standing on terra firma it reads 0. If it reads 100 knots you will be 100NM away from where you are now in one hour, so long as you keep flying ...

46

The Harrier, Yak-38, Yak-141, XV-15, and V-22 are all fixed wing aircraft. All can hover in mid air, controlled. So they are in controlled flight at 0 velocity. At least the Harrier can even be in controlled flight flying backwards, so with negative velocity. The others may as well, I don't know.

43

It is not a unit. It is just Microsoft trying to be funny. Or to convey an idea of the magnitude. Thanks @Jackie for pointing out that around March 2019, Microsoft has released this calculator as open source under MIT license. It is available in this Github repository. The source code sheds light on the definition of these pseudo units: Description in ./...

43

Because what determines the amount of lift generated is the indicated airspeed, not the ground speed. As usual, it is always easier to think about an extreme case. If you have an aircraft with VR (speed at rotation for takeoff) of 90 knots, and there is an 80 knots head wind, in theory it will rotate with ground speed of 10 knots even though the indicated ...

43

"Speed" is not a singular term in aviation. There are many different ways to measure speed. See for example Why is there a difference between GPS Speed and Indicator speed? Most commercial jets cruise with a true airspeed in the range 400-500 knots and an indicated airspeed in the range 200-300 knots. For the purpose of passenger transportation, ground ...

41

An airplane can slow down and reduce its speed while in flight. The easiest way to do so is to reduce the amount of thrust that the engines are producing. This will produce an almost immediate reduction of the airspeed, especially if the plane is maintaining the same altitude. There are also devices called air brakes and spoilers that can be further used ...

41

You can, but you have to live with the consequences. There are several things that can happen: Depending on the vertical gusts ahead, you might not even get close to v$_{NE}$. There is another speed limit for gusty weather called v$_B$, and exceeding this will run the risk of overstressing the wing structure. Going above v$_B$ will overstress the wings in a ...

35

A propeller accelerates the air of density $\rho$ which is flowing through the propeller disc of diameter $d_P$. This can be idealized as a stream tube going through the propeller disc: The air speed ahead is $v_0 = v_{\infty}$ and the air speed aft of the propeller is $v_1 = v_0 + \Delta v$. The propeller effects a pressure change which sucks in the air ...

33

It's an illusion that the blades appear to be going slowly. It's actually a well known effect called the wagon wheel effect. Essentially the rotor is spinning at close to an even multiple of the camera's framerate divided by the number of rotors. This means that between frames the blades have moved a full quarter rotation (or a multiple of that). Creating ...

33

No because aircraft are categorized by their speed at the runway threshold (1.3 times stall speed). VAT —Speed at threshold used by ICAO (1.3 times stall speed in the landing configuration at maximum certificated landing mass) By knowing the category, ATC is able to use appropriate speeds. The category is not actually listed anywhere, so the controller ...

32

The SR-71 was only capable of Mach 3.3 flight at altitude. You can see the limitations in the pilot's operating handbook(POH) for the aircraft: At higher altitudes the relative speed of sound is lower. If we use this handy NASA calculator in a standard atmosphere the relative speed of sound at 70,000 ft. is 660 MPH making your 2193 MPH equal to Mach 3.321 ...

31

Spoilers have many uses, but first I want to distinguish types of spoilers. Airplanes will typically have ground spoilers and flight spoilers and they work like they sound. Ground spoilers only open up on the ground -- these are usually much more detrimental to lift than the flight spoilers. Flight spoilers open when actuated by the pilots Another type of ...

31

At the critical mach number, some part of the aircraft (usually the wing) will have air flowing over it at a speed in excess of mach 1. If the aircraft is not meant to fly at transonic or supersonic speeds, shock waves will flow over the wing. This can either cause the wing to stall, the control surfaces to become unresponsive, or the plane to go into the ...

30

Your airspeed does not remain constant because of inertia: it takes more time for the airplane to adapt to the new relative wind, compared to the time it takes for the wind to change. Example One: you're flying 80 knots and the headwind is 20 knots. Over a time of 3 minutes, the headwind gradually reduces from 20 knots to 10 knots. Since the change is ...

30

The P&W PT6 comes in many different varieties. The smallest PT have 500hp while the largest have 1700hp. It is not the "same engine" as you state in your question. The standard Caravan has 675hp while the other aircraft you mention have 1,200hp. That alone can account for the major difference in performance. Fixed gear and struts also add to an ...

30

It won't be pleasant. The main result of being exposed outside at altitude, besides the obvious hypothermia, frostbite and hypoxia, will be bruising from the 280-ish knot slipstream (it's the indicated airspeed that matters as far was what you feel, not the true airspeed), and injuries from being flung around by any turbulent flow you are in. Most of your ...

29

Other than the TU-144 and Concorde, the record for the fastest True Airspeed in an airliner probably belongs to a DC-8. Wikipedia Douglas DC-8 On August 21, 1961, a Douglas DC-8 broke the sound barrier at Mach 1.012 (660 mph/1,062 km/h) while in a controlled dive through 41,000 feet (12,497 m) and maintained that speed for 16 seconds. The flight was to ...

28

No, it could not fly much faster with the available energy. Lift is a question of wing area and dynamic pressure. Solar Impulse 2 has 269.5 m² wing area to carry its 2.3 tons of mass. This is a wing loading of just 8.53 kg/m²; much less than even gliders have (they start at around 30 kg/m²). This allows it to fly very slowly; if we assume it ...

28

To reduce damage in case of a bird strike. The restriction is not only for the 737-100 and -200 models, the 737 NG QRH says: WINDOW HEAT OFF In flight: WINDOWS HEAT switch (affected window) ..... OFF Limit airspeed to 250 knots maximum below 10,000 feet. Pull both WINDSHIELD AIR controls. This vents conditioned air to the inside of the windshield for ...

26

It is not only the mass that affects the landing speed. Wing area plays an important role as well. A larger wing can lift more weight at the same speed than a smaller wing. If you compare the wing loading of these aircraft the differences are smaller: A388: Maximum landing weight: 391000 kg Wing area: 845 m2 Wing loading: 463 kg/m2 B744: Maximum ...

25

This answer is written for air transport category aircraft. Introduction During take-off there are three operationally significant speeds that ensure a safe take-off: V1 - the take-off decision speed VR - the rotation speed V2 - the take-off safety speed In addition there are three technically important speeds: VMU the minimum unstick speed VMCG the ...

24

Speed of a plane is actually measured in a number of different ways, and relative to different things. Here is a summary of the different types: Indicated Airspeed (IAS). This is the number shown on the instrument that measures airspeed, and isn't really relative to anything. Rectified Airspeed (RAS) or Calibrated Air Speed (CAS) This is IAS corrected for ...

23

Most modern jets use an Air Data Computer (ADC) to calculate (among other things) Mach Number. Air Data Computer An ADC is simply a computer which accepts measurements of atmospheric data to calculate various flight related data. A typical ADC may be connected to$^1$: Inputs Static System Pressure Pitot Pressure Total Air Temperature (TAT) Outputs (...

23

An (analog) machmeter looks something like this: So it's more like an more complex version of the airspeed indicator, in this case correcting for the altitude in the process. That being said, I found this extract apparently from an FAA publication: Some older mechanical Machmeters not driven from an air data computer use an altitude aneroid inside the ...

Only top voted, non community-wiki answers of a minimum length are eligible