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#12
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Bob: to your earlier post about some a/c starting rolling with brakes on:
well it's quite common on some types of a/c. The Reims Rocket, for example, at full throttle will jump on ahead no matter how much brakes you apply. During engine test, the only way we keep it from moving is to put massive chocks and tie the whole thing down (and if possible, rev it at the lowest speed possible for a successful test)... Types (strength) of brakes are fitted in relation to the landing speed and a/c MTOW - i.e. in relation to the kinetic energy and inertia the a/c has upon landing (simply speaking). They are not in relation (at least not directly) to engine power. So, if you, say, put a 250 HP engine into a Skyhawk, rev it up to max RPM and hold the brakes, it'll start edging forward slowly. Triple Delta "Bob Ingraham" wrote in message om... snip What approach speed do you use on that Spitfire. I'm supposed to watch my speed in addition to altitude, attitude, yaw, the horizon, and enjoy the scenery too? And then there's the question of German's lurking about, waiting to pounce on me. But I guess they'd probably have a hard time getting all the way to Vancouver.... ;^) Any, I certainly wasn't going very fast. I'd throttled back to about 1/3 power, had full flaps, and the approach was from a low altitude, not a power dive. Another question (I have lots of them, but I'll end with this one): I can barely get the Concorde to lift off the runway. It's hard to believe that the main runway at Vancouver isn't long enough. In fact, an actual Concorde visited Vancouver during Expo '86 and must have used that runway. Am I doing something wrong. There don't seem to be any flaps or controls for flaps. Do tail-less deltas even have flaps? I know Concorde has none. Are you sure you're using full thrust and no breaks. Also, what is your take-off speed? Remember that Sacremento ice cream store disaster of the early 1970's? snip No, I don't recall the ice cream store disaster. What happenened? I tried another takeoff and watched the speed dial. I was at 250 knots, and still sticking firmly to the runway, and then the mud flats, and then careering madly across Georgia Strait. X-Plane disasters are pretty silly. Bob |
#13
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A large delta aircraft like Concorde needs no flaps as the large wing
area traps a cushion of air beneath it and the ground during landing. Also the characturistic nose high attitude of deltas on landing not only provides hi lift but hi drag too. Perhaps when you was taking off in that Concord you allowed the nose to rise too high. Beleive it or not correct technique for take off in most deltas was to lift the nose wheel only a few feet from the runway and the aircraft would rise on attaining correct airspeed. |
#14
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On Wed, 8 Dec 2004 at 14:28:29 in message
.com, Les wrote: A large delta aircraft like Concorde needs no flaps as the large wing area traps a cushion of air beneath it and the ground during landing. Also the characturistic nose high attitude of deltas on landing not only provides hi lift but hi drag too. Perhaps when you was taking off in that Concord you allowed the nose to rise too high. Beleive it or not correct technique for take off in most deltas was to lift the nose wheel only a few feet from the runway and the aircraft would rise on attaining correct airspeed. Abridged Concorde Take off from book 'Flying Concorde' by Brian Calvert (Speeds only apply to the particular take off described). Afterburners are armed, clocks are started and throttles advanced to maximum. At 100 knots four greens showing full engine power and afterburners are confirmed. "Power checked" Decision speed (V1) is 165 knots At 192 knots 'Rotate' A tug on the column to lift the nose then a smooth rotation to 13.5 degrees nose up. During that the Concorde leaves the ground at 205 knots. It is held at 13.5 degrees nose up. V2 is confirmed at 221 knots. As the speed builds the nose is pulled up to 18 degrees. Then usually the nose is pushed down to 12 degrees, afterburners are cut and the throttles pulled back to a noise reducing setting maintaining a speed of 250 knots. -- David CL Francis |
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