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#91
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"Frijoles" wrote...
No, but the yaw indicator on the F-14 is! I've known generally what (the string) was for a long time but never bothered to ask when it was referenced (primarily)? High alpha stuff? Landing pattern? Single engine would be an obvious case...anything else? More for "departure prevention," TF 30 "management" or both? I never flew the Turkey, but probably all of the above. I flew gliders with them, and they replaced the turn balance ball -- "step on the knot". |
#92
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ok Jim... lets do a no flap approach...
IIRC.. I believe the airspeed and proper AoA will now be around 210.. correct.. BT B-1 GIB "Jim Baker" wrote in message ... Sorry, I thought it was clear I was speaking about AoA to fly final and land the Bone, as you said you use in the Harrier. "Frijoles" wrote in message ink.net... Good job JB, you compute an airspeed for the Bone. And so your point is...*what* about landing the Harrier? "Jim Baker" wrote in message news ![]() You're right Frijoles, in the Bone the correct answer for "What airspeed do you fly on final" is "I don't know/care. I'm flying 7 AoA as required by the Dash One". There is however, a chart of airspeed and gross weights that every pilot has and, IAW the Landing Checklist, every final must have an airspeed computed. JB "Frijoles" wrote in message ink.net... Nozzles aft, Harrier approach speed will be in the 155kt +/-range. At 20 nozzles and auto flaps(normal for IFR final), you're somewhat slower but to be honest I don't recall the airspeed because my primary reference was always AoA. Depending on the type of landing you intend to make, once you're in the visual environment, you transition to a higher nozzle angle (60-75 depending...), and in some instances, STOL flaps where the flaps program automatically as a function of nozzle angle. "On speed" for a fixed-nozzle slow landing is around 110kts. The *very* slow rolling landings you occasionaly see are called rolling vertical landings -- 60 kts ground speed is the target but the transition to that speed will usually be over the runway, not on approach final. "Darkwing Duck" wrote in message ... "Tetsuji Rai" wrote in message s.com... Airspeed limitation below 10000ft is usually 250kts unless you have been authorized by the Administrator. However I guess it's a bit slow for military fighters. So I am curious how fast military fighters fly in the real world. I guess it's very dangerous military aircraft fly much fast among civilian planes. So how fast is short final in a F-14 or whatever? Always wanted to know. |
#93
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Bill, as you no doubt remember, no flap approaches and landings were done at
6 AoA versus 7 AoA with flaps/slats. But the airspeeds for a no flapper were typically about 40 knots faster than with flaps/slats. You'd try to get down to about 20K lbs of fuel for a no flap landing which gave an approach/landing speed of 184 KIAS for a 210K lb. airplane. Cheers, Jim "BTIZ" wrote in message news:fs0Rb.61523$zs4.18646@fed1read01... ok Jim... lets do a no flap approach... IIRC.. I believe the airspeed and proper AoA will now be around 210.. correct.. BT B-1 GIB "Jim Baker" wrote in message ... Sorry, I thought it was clear I was speaking about AoA to fly final and land the Bone, as you said you use in the Harrier. "Frijoles" wrote in message ink.net... Good job JB, you compute an airspeed for the Bone. And so your point is...*what* about landing the Harrier? "Jim Baker" wrote in message news ![]() airspeed do you fly on final" is "I don't know/care. I'm flying 7 AoA as required by the Dash One". There is however, a chart of airspeed and gross weights that every pilot has and, IAW the Landing Checklist, every final must have an airspeed computed. JB "Frijoles" wrote in message ink.net... Nozzles aft, Harrier approach speed will be in the 155kt +/-range. At 20 nozzles and auto flaps(normal for IFR final), you're somewhat slower but to be honest I don't recall the airspeed because my primary reference was always AoA. Depending on the type of landing you intend to make, once you're in the visual environment, you transition to a higher nozzle angle (60-75 depending...), and in some instances, STOL flaps where the flaps program automatically as a function of nozzle angle. "On speed" for a fixed-nozzle slow landing is around 110kts. The *very* slow rolling landings you occasionaly see are called rolling vertical landings -- 60 kts ground speed is the target but the transition to that speed will usually be over the runway, not on approach final. "Darkwing Duck" wrote in message ... "Tetsuji Rai" wrote in message s.com... Airspeed limitation below 10000ft is usually 250kts unless you have been authorized by the Administrator. However I guess it's a bit slow for military fighters. So I am curious how fast military fighters fly in the real world. I guess it's very dangerous military aircraft fly much fast among civilian planes. So how fast is short final in a F-14 or whatever? Always wanted to know. |
#94
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You'd try to
get down to about 20K lbs of fuel for a no flap landing which gave an approach/landing speed of 184 KIAS for a 210K lb. airplane. Damn, and a 15,000'+ long runway ? BUFDRVR "Stay on the bomb run boys, I'm gonna get those bomb doors open if it harelips everyone on Bear Creek" |
#95
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![]() "BUFDRVR" wrote in message ... You'd try to get down to about 20K lbs of fuel for a no flap landing which gave an approach/landing speed of 184 KIAS for a 210K lb. airplane. Damn, and a 15,000'+ long runway ? It's not a big deal. Very landable (no hot brakes, not heroic efforts) with 8,000 ft rwy. As a matter of fact, you can land a min weight, configured Bone in about 3-4K feet. JB |
#96
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On Mon, 26 Jan 2004 00:53:22 GMT, "Frijoles"
wrote: I've known generally what (the string) was for a long time but never bothered to ask when it was referenced (primarily)? High alpha stuff? Landing pattern? Single engine would be an obvious case...anything else? More for "departure prevention," TF 30 "management" or both? We had a "yaw string" on F-4s in USAF. I don't recall if there was on for the F-105. The main purpose in operational aircraft was during weapons deliver and the most important weapons delivery with a yaw concern was strafe or rockets. Any yaw at the moment of release means the sight is pointing left or right of the flight path and the weapons will go in the direction the aircraft has imparted, not the place that the sight tells you. Yaw left, shoot right. Ed Rasimus Fighter Pilot (USAF-Ret) "When Thunder Rolled" Smithsonian Institution Press ISBN #1-58834-103-8 |
#97
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#98
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Damn, and a 15,000'+ long runway ?
It's not a big deal. Very landable (no hot brakes, not heroic efforts) with 8,000 ft rwy. Yeah, I realized that after I typed it. A 210K BUFF even without a drag chute would only eat up about 8,000' of runway, however in a 210K BUFF, you're on fumes! BUFDRVR "Stay on the bomb run boys, I'm gonna get those bomb doors open if it harelips everyone on Bear Creek" |
#99
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Boy, it's a mixture of fun and depression to talk about flying when you're
not actively doing it... Bit like sex. ROFLMAO...I could comment in any one of several ways here, but I'll choose to bow out gracefully ![]() BUFDRVR "Stay on the bomb run boys, I'm gonna get those bomb doors open if it harelips everyone on Bear Creek" |
#100
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Thanks -- had forgotten about sideslip and FF ordnance realignment with the
relative wind... "Ed Rasimus" wrote in message ... On Mon, 26 Jan 2004 00:53:22 GMT, "Frijoles" wrote: I've known generally what (the string) was for a long time but never bothered to ask when it was referenced (primarily)? High alpha stuff? Landing pattern? Single engine would be an obvious case...anything else? More for "departure prevention," TF 30 "management" or both? We had a "yaw string" on F-4s in USAF. I don't recall if there was on for the F-105. The main purpose in operational aircraft was during weapons deliver and the most important weapons delivery with a yaw concern was strafe or rockets. Any yaw at the moment of release means the sight is pointing left or right of the flight path and the weapons will go in the direction the aircraft has imparted, not the place that the sight tells you. Yaw left, shoot right. Ed Rasimus Fighter Pilot (USAF-Ret) "When Thunder Rolled" Smithsonian Institution Press ISBN #1-58834-103-8 |
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