![]() |
If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below. |
|
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]() "Bruce Hoult" wrote in message ... In article , Andy Blackburn wrote: Bruce's numbers are a pretty accurate rule of thumb. In an earlier thread there was some doubt expressed as to whether these 'theoretical' numbers can be achieved in flight. I took a look at some flight logs and found most of the time you convert into height ~90% of your kinetic energy (+/- the accuracy of my logger). There was one pull up where I only got 75% and one case where I got 100% (!). Best not to count on getting every last inch. Agreed, and thanks for the confirmation. Could headwind account for the 100% example? And tailwind for the 75%? In other words, your airspeed was not the same as your ground speed? -- Bruce | 41.1670S | \ spoken | -+- Hoult | 174.8263E | /\ here. | ----------O---------- I doubt it. More likely pulling up into rising/sinking air would account for the differentials. Frank Whiteley 40-26N 104-38W |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Aerobatics | 28 | January 2nd 09 02:26 PM |
AmeriFlight Crash | C J Campbell | Piloting | 5 | December 1st 03 02:13 PM |
Single-Seat Accident Records (Was BD-5B) | Ron Wanttaja | Home Built | 41 | November 20th 03 05:39 AM |
USAF = US Amphetamine Fools | RT | Military Aviation | 104 | September 25th 03 03:17 PM |
AOPA Stall/Spin Study -- Stowell's Review (8,000 words) | Rich Stowell | Piloting | 25 | September 11th 03 01:27 PM |