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Originally posted by weedwhacker
reply to post by weedwhacker
Oh, and an additional bonus if someone knows what kind of Sim that actually is, and where it's located. I will be watching closely, looking for clues (since I didn't see any credits for it).
If experienced pilots could not do this in a simulator....
Originally posted by weedwhacker
reply to post by QuidEstVerita
Ahhhhh....the keyword there is "IF"!!!:
If experienced pilots could not do this in a simulator....
The premise that experienced pilots "could not" do it is rubbish.
Hence, the thread premise is irrelevant. The "source" of the entire opening post (the "OP") is in quesiton, and needs to be evaluated properly.......
You could wear a helmet Weedwhacker like the guy on Top Gear.
We don't need faces, just controled results.
Originally posted by lachstockn2
At the risk of making myself look like an ignoranus, isn't the simulator rather useless in demonstrating aerodynamic stress levels on an airframe?
I realise the title of this thread implies that pilot skill is the pivotal issue, but personally I'm more interested in whether or not the aircraft itself is built to cope with those speeds under those conditions.
Not to discourage anyone from doing the experiment, though - I'm still interested in what the outcome might reveal.
Originally posted by lachstockn2
Wind tunnel testing is what I had in mind.
Anyone got access to one of those?
Even the REAL ignoramus (who used to post in this thread) admitted (once pressed) to the Boeing demonstrated 420 knots (KIAS) dive speed for the 767 (and, by default, the 757 as well....same "family").
And THAT was just for demo.....no reason aerdynamically that it could not go faster, in terms of KIAS.
Originally posted by weedwhacker
reply to post by lachstockn2
No, not an "ignoramus" for asking.
Originally posted by weedwhacker
reply to post by lachstockn2
Even the REAL ignoramus (who used to post in this thread) admitted (once pressed) to the Boeing demonstrated 420 knots (KIAS) dive speed for the 767 (and, by default, the 757 as well....same "family").
And THAT was just for demo.....no reason aerdynamically that it could not go faster, in terms of KIAS.
What is MOST CRITICAL on the airframe is the Mach number....especially nearing critical Mach, when airflow patterns on areas of the airframe can be HIGHER than the overall airplane speed.
Of course.....at the temperatures near Sea Level (as seen on 9/11) none of the airplanes got anywhere near Mach critical speeds.
... but isn't air density more relevant aerodynamically than air temperature at such a low altitude? Isn't that why they refer to KEAS (Knots Equivalent Air Speed) in this type of scenario?