![]() |
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 |
#51
|
|||
|
|||
![]()
Dudley Henriques wrote in
: Bertie the Bunyip wrote: Dudley Henriques wrote in news:J6mdnf- : Bertie the Bunyip wrote: "Private" wrote in : "Dudley Henriques" wrote in message ... It's interesting to note that although stall recovery should be thought of as something done with a minimum loss of altitude, the emphasis on recovery should always be placed on the regaining of angle of attack as PRIME to recovery. Agreed, I have always thought of myself as flying a wing to which is attached a fuselage rather than the reverse. Xactly right IMO. All you need is a wing to fly, after all. Bertie As you already know and I can confirm emphatically , as soon as you start flying high performance jets, it's all about wing management. Actualy, in the turkeys we fly it's all about nailing your pitch to what the computer wants, but you're right, they're all about the wing. I've always understood that to be the case, but I learned to fly in gliders, so it was more about pefromance and less about procedure like it is in a lot of lightplane instruction. Bertie In the T38 for example, the approach is flown at an optimum alpha on the indexer or at a specific airspeed plus fuel. Either way, the object is to keep the wing within specific limits aoa wise. The bird will develop a sink rate that can't be recovered otherwise. I've always wondered why you guys in the big jets don't use alpha more on the approach. I'm guessing it's because of the complicated fuel loads possible which gives you such a wide range of approach speeds to bug to keep the pitch angle right at touchdown. I know that Boeing for one is doing some research into providing better aoa data to you on the ADI for approaches but haven't heard much about how this outreach is being accepted by the carriers. Well, the military guys have it. I was in a 141 sim once and that had it. We bug a diffeent approach speed for each weight. The takeoff speeds provide for a variety of AoAs depending on whether we want to climb, get off a short runway or get over some obstacles. We can select a range of V2s based on a runway analysis to get the most weight possible off the ground on a given takeoff. That, of course, gives us different AoAs depending on whether we're looking for best angle or best rate. We don't call it any of that, but it's exaclty what we do. on approach we select Vso 1.3 based on the weight. So we do use a constant alpha. It's important to avoid float, and to touch down at the right attitude so we don't end up bouncing off the nosewheel or the tail as well. I do it in light planes as well, and hopefully most guys do have nominal approach speeds for different weights.. I just knock off a few knots if I'm light, basically. Bertie Bertie |
#52
|
|||
|
|||
![]()
On Feb 16, 4:41 pm, Bertie the Bunyip wrote:
wrote : On Feb 15, 6:37 pm, Bertie the Bunyip wrote: "Robert M. Gary" wrote in news:ebb74b75-9910-4c50-ae86- : On Feb 15, 3:56 pm, Dudley Henriques wrote: Bertie the Bunyip wrote: Dudley Henriques wrote in : Man there are a lot of posts on this topic. Too much newsgrouping, people need to do more flying ![]() When my airplane is finished! Bertie Watchu building? A Hatz, but it's a Citabria being restored I'm waiting to fly. Bertie Cool. Thanks. My son took a Young Eagle flight last year in a Citabria...after flying FsX. He loved it. |
#53
|
|||
|
|||
![]()
On Feb 16, 4:44 pm, Bertie the Bunyip wrote:
wrote : On Feb 15, 9:54 pm, Bertie the Bunyip wrote: wrote innews:48ff8b66-f84b-4281-998b-158e7acf78dd@ 28g2000hsw.googlegroups.co m: On Feb 15, 9:06 pm, wrote: The ultimate answer to getting the quality level up in the GA pilot community will in my opinion require a whole new look at the way flight instruction is conducted. ... Dudley Henriques Obliquely related to the topic of comfort in the left hand curve of the flight envelope, some low speed F22 aerobatics: http://www.airventure.org/2008/news/080214_raptors.html What a ride that aircraft provides. Well, that thing looks after alpha for you. Bertie OH that's just great. Now I have to ask WTF 'alpha' is. ****. Thanks. ;-) Sew watt is it? Oh sorry, slang for Angle of Attack, basically. Bertie Ahhh... a 'docile' well centered ac. Similar to a non-elliptical airfoil parachute. (Like mine, being old, slow and ready to live till the end of the week). Richard. |
#54
|
|||
|
|||
![]() |
#56
|
|||
|
|||
![]()
On Sat, 16 Feb 2008 22:44:08 +0000 (UTC), Bertie the Bunyip
wrote: wrote in : On Feb 15, 9:54 pm, Bertie the Bunyip wrote: wrote innews:48ff8b66-f84b-4281-998b-158e7acf78dd@ 28g2000hsw.googlegroups.co m: On Feb 15, 9:06 pm, wrote: The ultimate answer to getting the quality level up in the GA pilot community will in my opinion require a whole new look at the way flight instruction is conducted. ... Dudley Henriques Obliquely related to the topic of comfort in the left hand curve of the flight envelope, some low speed F22 aerobatics: http://www.airventure.org/2008/news/080214_raptors.html What a ride that aircraft provides. Well, that thing looks after alpha for you. Bertie OH that's just great. Now I have to ask WTF 'alpha' is. ****. Thanks. ;-) Sew watt is it? Oh sorry, slang for Angle of Attack, basically. Bertie ************************************************** ******************* Bertie Just tell him that when thrust exceds gross weight, Alpha no longer is a problem. Big John |
#57
|
|||
|
|||
![]()
Big John wrote in
: On Sat, 16 Feb 2008 22:44:08 +0000 (UTC), Bertie the Bunyip wrote: wrote in news:5268d2a1-66db-4dd9-8616-6defa1a7cab2 @n58g2000hsf.googlegroups.com: On Feb 15, 9:54 pm, Bertie the Bunyip wrote: wrote innews:48ff8b66-f84b-4281-998b-158e7acf78dd@ 28g2000hsw.googlegroups.co m: On Feb 15, 9:06 pm, wrote: The ultimate answer to getting the quality level up in the GA pilot community will in my opinion require a whole new look at the way flight instruction is conducted. ... Dudley Henriques Obliquely related to the topic of comfort in the left hand curve of the flight envelope, some low speed F22 aerobatics: http://www.airventure.org/2008/news/080214_raptors.html What a ride that aircraft provides. Well, that thing looks after alpha for you. Bertie OH that's just great. Now I have to ask WTF 'alpha' is. ****. Thanks. ;-) Sew watt is it? Oh sorry, slang for Angle of Attack, basically. Bertie ************************************************** ******************* Bertie Just tell him that when thrust exceds gross weight, Alpha no longer is a problem. So I've heard, but never got the chance to try it! Well, with an RC model, maybe...But not strapped to one! Bertie |
#58
|
|||
|
|||
![]()
Dudley Henriques wrote in
: Ken S. Tucker wrote: On Feb 16, 2:08 pm, "Private" wrote: "Ken S. Tucker" wrote in oups.com... As much as I like the "dud" his post is the most completely idiotic thing I had to read. On Feb 16, 12:10 pm, Dudley Henriques wrote: It's interesting to note that although stall recovery should be thought of as something done with a minimum loss of altitude, the emphasis on recovery should always be placed on the regaining of angle of attack as PRIME to recovery. NUTZ. You need airspeed, it's called kinetic energy that is needed to suck off, using the wings (you know, those little things that protude out the side of airplanes). I am one instructor who strongly believes that instructors should consider altering their approach to teaching stall to focus more strongly on recovering angle of attack than recovering in minimum altitude. See KIAS, Dud, you'd last 2 minutes in the RHS of my plane, after that you'd be lickin' pavement, from my shoe on your ass. Stalls entered at low altitude have many times resulted in secondary stall entry or a mushed recovery followed by ground impact by pilots who COULD have lowered the nose and held it down there a bit longer than they did, using the air under them to better advantage and giving themselves the needed time to regain angle of attack and smooth airflow as they attempted a recovery. But because they had been taught that ALTITUDE rather than AOA was the killer, they recovered trying to save altitude, when in reality what was needed was to USE THE AVAILABLE ALTITUDE CORRECTLY....and save the airplane. Toward this goal, I strongly encourage all CFI's to reference AOA in stall recovery. This doesn't mean INSTEAD of altitude, but it does mean that to recover the airplane, you absolutely HAVE to restore AOA, and at low altitude that might very well mean using available altitude to the last foot of air to do that. I have always taught stall recovery both with and without power. The FAA requires power. I want the student to see the difference and at the same time be able to stress that it's the ANGLE OF ATTACK that saves your butt. The strong lesson here is that you USE altitude......you don't try to minimize it at the expense of angle of attack. Dud, you're clueless, you have not a clue about KIAS, spiral dives or g-force recovery's. In short I see NO evidence you have even been in an airplane with your focus on AoA. I can get a good AoA at 10 KIAS or 200 KIAS, what are going to do? Regards Ken Ken, With respect, I think you must have missed my reply in another thread. I am enclosing it here for your convenience and consideration. "Private" wrote in message ... "Ken S. Tucker" wrote in message om... I was out paying taxes, to get some coin for the piggy bank, I shook it 3 times and still didn't hear any rattling, that's simple accounting to tell me when I'm broke, works every time! Ken Some here would suggest that you apply the same strategy to your head before posting. I am somewhat embarrassed to be entering this thread, but I just can't resist swinging at a soft pitch like that. Happy landings, To elaborate, my suggestion was that before posting you should give your head a shake to determine if there is anything inside and to consider whether you really wished to make the fact public. Happy landings, If I were you, I'd ****-off and read. You're swinging at screw-balls... Me and the "dud" ****ed your mush mind. Get a ****in life, crack a book. Best Regards Ken xxxx Just for the record, and on the off chance that there might just be one person on Usenet who needs to be informed of this, please be advised that regardless of what this idiot says and when he uses my name in his posts; I am in NO way even remotely involved with this character in any way whatsoever. It should be obvious that Ken always puts the "S" between "Ken" and "Tucker" to emphasize to everyone that he is a total ****HEAD! |
#59
|
|||
|
|||
![]()
Bertie the Bunyip wrote:
Dudley Henriques wrote in : Bertie the Bunyip wrote: Dudley Henriques wrote in news:J6mdnf- : Bertie the Bunyip wrote: "Private" wrote in : "Dudley Henriques" wrote in message ... It's interesting to note that although stall recovery should be thought of as something done with a minimum loss of altitude, the emphasis on recovery should always be placed on the regaining of angle of attack as PRIME to recovery. Agreed, I have always thought of myself as flying a wing to which is attached a fuselage rather than the reverse. Xactly right IMO. All you need is a wing to fly, after all. Bertie As you already know and I can confirm emphatically , as soon as you start flying high performance jets, it's all about wing management. Actualy, in the turkeys we fly it's all about nailing your pitch to what the computer wants, but you're right, they're all about the wing. I've always understood that to be the case, but I learned to fly in gliders, so it was more about pefromance and less about procedure like it is in a lot of lightplane instruction. Bertie In the T38 for example, the approach is flown at an optimum alpha on the indexer or at a specific airspeed plus fuel. Either way, the object is to keep the wing within specific limits aoa wise. The bird will develop a sink rate that can't be recovered otherwise. I've always wondered why you guys in the big jets don't use alpha more on the approach. I'm guessing it's because of the complicated fuel loads possible which gives you such a wide range of approach speeds to bug to keep the pitch angle right at touchdown. I know that Boeing for one is doing some research into providing better aoa data to you on the ADI for approaches but haven't heard much about how this outreach is being accepted by the carriers. Well, the military guys have it. I was in a 141 sim once and that had it. We bug a diffeent approach speed for each weight. The takeoff speeds provide for a variety of AoAs depending on whether we want to climb, get off a short runway or get over some obstacles. We can select a range of V2s based on a runway analysis to get the most weight possible off the ground on a given takeoff. That, of course, gives us different AoAs depending on whether we're looking for best angle or best rate. We don't call it any of that, but it's exaclty what we do. on approach we select Vso 1.3 based on the weight. So we do use a constant alpha. It's important to avoid float, and to touch down at the right attitude so we don't end up bouncing off the nosewheel or the tail as well. I do it in light planes as well, and hopefully most guys do have nominal approach speeds for different weights.. I just knock off a few knots if I'm light, basically. Bertie Bertie I've always said that if I could only have one instrument in the airplane I'd like an angle of attack indicator. :-)) In a way we have the same problems landing in airplanes like the T38 as you do in the big jobs. We usually are dealing with a long fuselage mass to wing mass configuration in the fast jets that requires a specific aoa spread at touchdown to keep from catching the tail feathers. The F104 was particularly susceptible to this. (never flew the zipper but always wanted to). The F14 and the F16 (have flown these) are a narrow alpha spread at touchdown. The approaches in these airplanes all require strict wing management right down to the ground. With you guys, the GW can be so wide an available spread that flying an optimum aoa would probably put you outside your landing allowance spread to clear your tails if I understand correctly. This makes sense anyway, considering how long some of the stuff is you guys are handling. -- Dudley Henriques |
#60
|
|||
|
|||
![]()
Dudley Henriques wrote in
news ![]() Bertie the Bunyip wrote: Dudley Henriques wrote in : Bertie the Bunyip wrote: Dudley Henriques wrote in news:J6mdnf- : Bertie the Bunyip wrote: "Private" wrote in : "Dudley Henriques" wrote in message ... It's interesting to note that although stall recovery should be thought of as something done with a minimum loss of altitude, the emphasis on recovery should always be placed on the regaining of angle of attack as PRIME to recovery. Agreed, I have always thought of myself as flying a wing to which is attached a fuselage rather than the reverse. Xactly right IMO. All you need is a wing to fly, after all. Bertie As you already know and I can confirm emphatically , as soon as you start flying high performance jets, it's all about wing management. Actualy, in the turkeys we fly it's all about nailing your pitch to what the computer wants, but you're right, they're all about the wing. I've always understood that to be the case, but I learned to fly in gliders, so it was more about pefromance and less about procedure like it is in a lot of lightplane instruction. Bertie In the T38 for example, the approach is flown at an optimum alpha on the indexer or at a specific airspeed plus fuel. Either way, the object is to keep the wing within specific limits aoa wise. The bird will develop a sink rate that can't be recovered otherwise. I've always wondered why you guys in the big jets don't use alpha more on the approach. I'm guessing it's because of the complicated fuel loads possible which gives you such a wide range of approach speeds to bug to keep the pitch angle right at touchdown. I know that Boeing for one is doing some research into providing better aoa data to you on the ADI for approaches but haven't heard much about how this outreach is being accepted by the carriers. Well, the military guys have it. I was in a 141 sim once and that had it. We bug a diffeent approach speed for each weight. The takeoff speeds provide for a variety of AoAs depending on whether we want to climb, get off a short runway or get over some obstacles. We can select a range of V2s based on a runway analysis to get the most weight possible off the ground on a given takeoff. That, of course, gives us different AoAs depending on whether we're looking for best angle or best rate. We don't call it any of that, but it's exaclty what we do. on approach we select Vso 1.3 based on the weight. So we do use a constant alpha. It's important to avoid float, and to touch down at the right attitude so we don't end up bouncing off the nosewheel or the tail as well. I do it in light planes as well, and hopefully most guys do have nominal approach speeds for different weights.. I just knock off a few knots if I'm light, basically. Bertie Bertie I've always said that if I could only have one instrument in the airplane I'd like an angle of attack indicator. :-)) In a way we have the same problems landing in airplanes like the T38 as you do in the big jobs. We usually are dealing with a long fuselage mass to wing mass configuration in the fast jets that requires a specific aoa spread at touchdown to keep from catching the tail feathers. The F104 was particularly susceptible to this. (never flew the zipper but always wanted to). The F14 and the F16 (have flown these) are a narrow alpha spread at touchdown. Yeah, I could well imagine with an airfoil like that. The approaches in these airplanes all require strict wing management right down to the ground. With you guys, the GW can be so wide an available spread that flying an optimum aoa would probably put you outside your landing allowance spread to clear your tails if I understand correctly. This makes sense anyway, considering how long some of the stuff is you guys are handling. Well, it depends on what you mean by optimum. I presume you're talking about maintaining a healthy enough Alpha to prevent a departure, then controllability, and finally due consideration to touchdown attitude. I know most of the fast jet guys I fly with can't do a crosswind landing worth a damn! They fly a straight line down to touchdonw ( good) then pull the taps closed, yank and close their eyes. It seems to work but it ain't pretty! We fly most of them just like airplanes, really. Bertie |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
Stall Recovery | Danny Deger | Piloting | 12 | January 30th 07 01:01 AM |
stall strips ??? | Tri-Pacer | Owning | 6 | December 8th 06 06:18 PM |
Bad place to stall | Stubby | Piloting | 23 | June 21st 05 04:10 PM |
Wing Stall | PaulaJay1 | Owning | 18 | December 11th 03 07:46 PM |
Stall resistant 172? | Roger Long | Piloting | 19 | October 18th 03 11:48 PM |