Welcome to Flightinfo.com

  • Register now and join the discussion
  • Friendliest aviation Ccmmunity on the web
  • Modern site for PC's, Phones, Tablets - no 3rd party apps required
  • Ask questions, help others, promote aviation
  • Share the passion for aviation
  • Invite everyone to Flightinfo.com and let's have fun

Vx and Vy

Welcome to Flightinfo.com

  • Register now and join the discussion
  • Modern secure site, no 3rd party apps required
  • Invite your friends
  • Share the passion of aviation
  • Friendliest aviation community on the web

uwochris

Flightinfo's sexiest user
Joined
Dec 21, 2001
Posts
381
Hey guys,

Can someone please explain why Vy decreases with altitude while Vx increases with altitude? I have yet to find an explanation for this, not even in the Advanced Pilot's Manual (at least I could never find one there).

TIA.
 
the Advanced Pilot's Manual

If it's Kershner's book you have try chapter 6.
 
Try this one for a lay explanation:

Vy is based on how much power you have in excess of the amount of power you have to maintain straight and level flight. Think about flying straight and level at 70 kts in a 172. Very little power is needed. Increase power, maintaining the 70 kts, and you climb. More power, higher rate of climb. Vy is the airspeed at which the difference between power available and power required for straight and level flight is the greatest. As you increase in altitude, there is less power available, so the airspeed at which the difference is the greatest goes down.

On the other hand, Vx is based on available thrust. Vx is the airspeed in which the greatest amount of thrust is available. An airplane with virtually unlimited thrust could fly straight up and the distance it can climb within a set horizontal distance be "infinite" (very loosely speaking). Think of our cartoon view of a rocket ship - straight up to outer space with no horizontal movement at all - forward airspeed is zero. (Of course, we don't fly airplanes that go straight up, but it helps visualize the concept.) As altitude increases, the amount of thrust also decreases - less power available to produce the thrust, more propeller "slippage" as air density gets thinner, etc. So, the airplane can't go straight up any more. In order to climb, we now have to lower the nose. Which in turn means an increase in airspeed.
 
If you have access to the old "FTH" Flight Training Handbook, the information is on page 308.
 

Latest resources

Back
Top