Wolfgang Langewiesche didn't teach V speeds, but rather gaits. Because engines were not as reliable in his day and the Stromberg carburetor tended to flood with rapid throttle movement, his stall down approach technique (302-304) was the apparent brisk walk rate of closure approach with the throttle closed. The actual power pitch approach was reserved for larger airplanes with better carburetors. This was why he said the stall down approach was more difficult than the round out and hold off approach, also with the throttle closed. Better engines brought the fourth control into the mix, the throttle. Both approach techniques became easier with addition of the fourth control, but the apparent brisk walk rate of closure approach from a 600' up and a quarter mile out became a snap. It became the premier short field technique.
While not using the V designation, Wolfgang talks about climbing at both the fastest up gait and the most up over distance gait. He doesn't have much use for either, preferring level acceleration and zoom climb. So this fortnight hopefully we can come to agreement on the advantages and disadvantages of both techniques...the airspeed over altitude argument.
Vx or Vy as appropriate advantages...the altitude over airspeed argument:
Most up over distance or fastest up mathematically.
Integrated instrument manageable.
Down drainage egress not necessary.
Easy to evaluate for testing.
Most vertical space available.
Vx or Vy as appropriate disadvantages:
Slower and thus more dependent on stable conditions.
Absolute nearest to out of ground effect stall airspeed.
Integrated instrument dependent.
Tremendous amount of ground effect energy wasted by climbing out sooner than absolutely necessary.
Tremendous amount of down drainage energy wasted by climbing out sooner than absolutely necessary.
Evaluation (school solution)=primacy of less efficient technique.
Absolute least maneuvering airspeed available.
Absolute highest pitch attitude and most pitch down necessary to recover from a stall.
Much too low to recover from inadvertent stall.
More possibility of upset or LOC and uncontrolled flight into terrain (stall.)
Outcome of rush to altitude often in question?
Inadvertent stall mostly fatal.
Basic low ground effect takeoff and down drainage egress advantages...the airspeed over altitude argument:
Best use of all energy available, ie low ground effect over all unobstructed surface, no kinetic energy wasted overflying obstructions higher than necessary, and down drainage egress possible with maneuvering airspeed.
Doesn't require inside the cockpit instrument distraction.
Fastest airspeed possible for safe maneuvering including ability to miss some obstructions horizontally.
Least possibility of inadvertent stall.
Least pitch attitude except for temporary zoom climb as necessary.
Least possibility of upset, LOC, or uncontrolled flight into terrain (stall.)
Outcome of cruise climb never in question.
Basic low ground effect takeoff and down drainage egress disadvantages:
Least vertical space available.
Doesn't promote instrument integration.
Doesn't allow mechanical testing. Bot doesn't do art.
More possibility of CFIT. Wolfgang says hitting terrain is actually safer than falling into terrain head first.
Inadvertent stall mostly fatal.
Wolfgang taught airspeed is altitude and altitude is airspeed (the law of the roller coaster,) but preferred airspeed when too low to recover from inadvertent stall. He said altitude was money in the bank, but airspeed was money in your pocket. That says a lot to me. Experience of eleven non injury engine failures below 200' with zoom reserve airspeed has made me a believer in money in my pocket.
So what are your thoughts and experiences? Has less than 1,000' been enough to recover from inadvertent stall for anyone you know? Where was it not enough? How do stall on the approach fatalities compare to stall on takeoff and turn to crosswind fatalities? How is mushing on short final different than mushing after takeoff (think fourth control?) Is learning to fly the razor's edge of stall, or believing recovery is possible, more important than teaching avoidance and using designed safety features? Can the airplane stall itself if we refuse to pull back on the stick?
So what is both safe and practical? I had the advantage of training pilots at mostly spray strips and uncrowded uncontrolled airports. Almost all of the six hours to prepare for solo was circuits. We did ten each hour because there was no need to go all the way up to 1,000,' in a 65 hp airplane. And at 60 mph top speed there was no need to go further than 1/4 mile out in the pattern, including final. The basic low ground effect takeoff gave us maneuvering airspeed. The nose was allowed to go down naturally in all turns. Most slow flight was conducted in low ground effect over the runway well below Vso because that is the gait of landing. Energy management and the law of the roller coaster was taught because recovery from inadvertent stall was not possible. The apparent brisk walk rate of closure approach was taught because it was the easiest and safest approach. Leading rudder was taught because old 65 hp airplanes didn't turn the right way without slipping using the primary aileron and pull back technique. So was I crazy to think they would be able to sort things out at altitude allowing recovery from inadvertent stall with less time spent up there? Was I crazy to emphasize low altitude maneuvering flight? Does the less time in the pattern than up high over an aviation career justify no energy management training at low altitude?
How do we unindoctrinate students in the primacy of altitude? How do we convince them that Vx or Vy as appropriate is just a suggestion and is mostly not appropriate? How do we make them give up airspeed reluctantly, carefully, questioning the reason why? How do we make them believe we don't want them to spend all the money in their pocket in a rush to the bank? How do we make them feel, in their bones, that the airplane will not necessarily climb?
