More Flaps = More Power = More Noise.
Years ago when I flew a Falcon 20 into Jackson Hole I had to send a fax saying we would not land with full flaps so it would be quieter.
The reduced flap settings for stage III along with the engine mods allow the plane to be a little quieter, since you don't have to carry as much power with flaps 25, 28, or 30. With flaps 40 you have to carry a lot more power/noise during the approach due to the greatly increased drag. I have also been told that flaps 40 would growl or whistle when used. I have usued 40 so I can't tell you if that is true or not.
Orange Anchor can you comment of Flaps 40. I am sure you were of the generation that could use them.
Great video thanks
The reduced flap settings for stage III along with the engine mods allow the plane to be a little quieter, since you don't have to carry as much power with flaps 25, 28, or 30. With flaps 40 you have to carry a lot more power/noise during the approach due to the greatly increased drag. I have also been told that flaps 40 would growl or whistle when used. I have usued 40 so I can't tell you if that is true or not.
Great video thanks
Stage I and II turbojets still rule.
Well, you don't necessarily need/require water injection for a straight turbojet engine.
Okay, then why did some use water injection and others didn't. What're the pros and cons if any?
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To increase thrust on hot days, some mil aircraft used water injected into the compressor inlet for non-afterburning engines. Pros, increased thrust by about 20-30%, since the water allows the inlet air to be cooled and thus increases its density, allowing for more fuel to be burned. Cons, weight of lugging the water, desalinization plants needed for it, and logisitcs of using it. The B-52 went from something like 11,000 lbs thrust without it, to 13,500+ with water injection. Normally only used for takeoff.
Turbojet engines have no bypass such that turbofans do (no fan in front), and their compressor/turbine share the same shaft using the velocity of the exhaust gas directly to produce. Noisy and fairly fuel inefficient, but cool.....essentially what goes in, goes through the combustion chamber and goes out back, versus some being bypasses around the engine core, such as low/high bypass turbofans do. GE CJ-610 (Lear 23), P&W JT12 (Lockheed Jetstar), and J60 (NAA Saberliner) are good examples of these.
The 60 Saberliner was fun to fly but hard to make it go very far. In the GE Falcon 20 we could push about 85K of wind from LGA to DAL. Pushed 150K of wind one day out of DCA back to DAL but the weather was good in DAL. 60 Saber never would have made it.
That sucks, because I love the Saberliner series.......cool looking design.
I only flew the 60. From what I had heard the 65 has a much greater range but does not fly as well. Again from what I have heard the 80 is the best overall. The 80 has the same engines as the Falcon 20 but it is much lighter.
Turbojets. Are those the LOUD engines that used water injection, and had the large black plooms of smoke escaping out the rear?
The reduced flap settings for stage III along with the engine mods allow the plane to be a little quieter, since you don't have to carry as much power with flaps 25, 28, or 30. With flaps 40 you have to carry a lot more power/noise during the approach due to the greatly increased drag. I have also been told that flaps 40 would growl or whistle when used. I have usued 40 so I can't tell you if that is true or not.
Orange Anchor can you comment of Flaps 40. I am sure you were of the generation that could use them.
To increase thrust on hot days, some mil aircraft used water injected into the compressor inlet for non-afterburning engines. Pros, increased thrust by about 20-30%, since the water allows the inlet air to be cooled and thus increases its density, allowing for more fuel to be burned. Cons, weight of lugging the water, desalinization plants needed for it, and logisitcs of using it. The B-52 went from something like 11,000 lbs thrust without it, to 13,500+ with water injection. Normally only used for takeoff.
Turbojet engines have no bypass such that turbofans do (no fan in front), and their compressor/turbine share the same shaft using the velocity of the exhaust gas directly to produce. Noisy and fairly fuel inefficient, but cool.....essentially what goes in, goes through the combustion chamber and goes out back, versus some being bypasses around the engine core, such as low/high bypass turbofans do. GE CJ-610 (Lear 23), P&W JT12 (Lockheed Jetstar), and J60 (NAA Saberliner) are good examples of these.
All our birds have a mod for Stage III. The majority fleet only uses Flaps 25 with the two odd balls using 30 or 28.
I wish we had some Super 72's as it would be nice to have the -217's or 200's on the pods. However, we are fourtnate that the smallest engine we have are -9A's. I have heard the war stories of guys flying the -7Bs out of Vegas and what a PITA those planes where.
Wow, a YS-11, that looks like it is an interesting plane to fly. There are a few of them sitting down in Laredo, TX.
we had -7, -9 and -15 engines with an intermix approved. The USAir birds, which I never flew, had the -17 engines.
I did get to fly the 727 in the FEDEX mod which I think had 2 -217s and a -17 in the center and a 727-100 with 2 -217s on the pod and a -7 in the center. It was as if they added a 4th engine and you could climb above the wing's ability.. or so it seemed.
The YS-11 was one odd duck. Water injection, 2 16ft props and a wicked flare required for a good landing. But it would haul 48 pax out of ROA, BLU, and Huntington with no problem.
When I got hired at PI I went to some of my USAF buddies still on active or reserve and pulled a big set of the mil charts and put them in my flt kit. We seldom got above 10,000 and so I would pull out those charts and follow the flight via ground ref. One of the old grumpy SOBs asked one day what the hell I was doing. I said I was just following the flight via landmarks and he asked why. I said I had never flown anything that far and that low routinely.. that most of my time was above a reset of 29.92. That remark came back to bite me. This was all prior to the big onset of CRM and some capts were textbook.