I think that's a Halifax. The air scoop on the top is similar to that of the Short Stirling too though. Here's a picture of a Halifax: https://th.bing.com/th/id/OIP.C5VAw9F_WasuV2Tj9FxfGwHaE8?pid=ImgDet&rs=1
Here's a link to an image of a Short Stirling...
I think the 1.36 CL max is the number they got trimmed for best glide engine off. Descending of course, it would generate a low lift. The highnumber would be for the number achieved at MAX AOA and full throttle.
The high number is just a bit higher than I got with a basic calculation of MAX CL...
The RAE contended in Technical note no.aero.1106 dated March 1943
That the NACA testers used a less accurate method. I've attached a jpeg of the document.
Here's something to try - I'm going to have a go later this week- using the same wing area and weight, calculate what the stall speed would...
Another error: The idea of a no warning stall in the Spitfire.
All the spits had ample buffet warning of the stall, and NACA reports argue that the Spit V could be flown 'partly stalled'.
The body should be laid to rest where the family decides.
The war ended a long time ago and wartime conventions, while important and certainly still respectful of the deceased- need not be slavishly adhered to.
Odd, If i remember Brown's account properly, they opened assymetrically on him when he was behind a p51. But I may well be misremembering it. I'll have to re-read his account when I get home this weekend.
And slipstream effect can, as you suggest, affect other traiing aircraft profoundly.
My...
Where you really see a quantitative advantage for the F4u is the dash 4 and later, the Dash 5.
Astonishing rates of climb and top speed.
Keep up the good work HoHun! - us grognards dig it.
finnster
HI Henning- good info!
If I'm reading the chart correctly(and there's no guarantee of that!) the 109's infinitely variable flap should allow 20 degrees at up to 450km/hr? I wonder how long that would take to deply (how many turns of the wheel) and how much the pressure required to turn the...