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Old 14th Aug 2010, 17:38
  #1890 (permalink)  
HazelNuts39
 
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Originally Posted by D Bru
Interesting reference to the V/S article in support of a “deep stall” scenario. Thanks, mm43. On the face of it doesn’t sound as improbable as that. Having said that, I cannot really follow all the mumbo-jumbo calcs.
Just to confuse you a bit more, I think mr. Squair's numbers should read:

* hcbn = 7350 – 750 ft/min X 251/60 = 7350 ft - 3138 ft = 4212 ft

Now as a 2.03625437 inHg pressure change gives approximately a 2036 ft altitude change, and as the external pressure is 1 psi more than the cabin pressure (3), the external or aircraft altitude (hacft) is simply:

* hacft ≈ 4212 - 2036 ft = 2176 ft

2:14:21 - 2:15:14 = 53 sec

rate of descent = 2463 fpm

regards,
HN39

Last edited by HazelNuts39; 15th Aug 2010 at 09:55. Reason: typo
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