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For the real engineers here



 
 
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  #1  
Old June 25th 08, 06:56 PM posted to rec.aviation.piloting
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Posts: 181
Default For the real engineers here

I'm thinking of a clean glider, one that might weigh 1500 pounds and
has a glide angle of say 1 in 25. At 50 miles an hour, that would mean
in an hour's time it might descend two miles (of course scale it
reasonable numbers, I chose those for ease of calculation). That means
it's losing about 1500 * 5280 * 2, or about 16 million foot pounds of
energy an hour.

Now if I add an engine swinging an 8 foot diameter prop, maybe as a
pusher, the question is, how big an engine for cruise only? A
horsepower is 550 foot lbs a second, or about 2 million foot pounds
an hour. If all of that is correct, it suggests with a 50% efficient
prop a little 16 horsepower engine could pretty much keep this thing
at constant altitude.

It passes the reasonableness test as far as I can see. Any serious
disagreements?

For those of you who do things in metric units? I went to school a
long long time ago, and here in the US I can buy a little Briggs and
Stanton (spelling?) engine with a horsepower rating, not a kilowatt
one.
  #2  
Old June 25th 08, 07:10 PM posted to rec.aviation.piloting
Bertie the Bunyip[_24_]
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Posts: 2,969
Default For the real engineers here

wrote in news:f21210b7-96ff-44c6-9b4b-120e489e7682@
59g2000hsb.googlegroups.com:

I'm thinking of a clean glider, one that might weigh 1500 pounds and
has a glide angle of say 1 in 25. At 50 miles an hour, that would mean
in an hour's time it might descend two miles (of course scale it
reasonable numbers, I chose those for ease of calculation). That means
it's losing about 1500 * 5280 * 2, or about 16 million foot pounds of
energy an hour.

Now if I add an engine swinging an 8 foot diameter prop, maybe as a
pusher, the question is, how big an engine for cruise only? A
horsepower is 550 foot lbs a second, or about 2 million foot pounds
an hour. If all of that is correct, it suggests with a 50% efficient
prop a little 16 horsepower engine could pretty much keep this thing
at constant altitude.

It passes the reasonableness test as far as I can see. Any serious
disagreements?

For those of you who do things in metric units? I went to school a
long long time ago, and here in the US I can buy a little Briggs and
Stanton (spelling?) engine with a horsepower rating, not a kilowatt
one.


Here ya go...

http://www.usenet.com/newsgroups/rec.../msg06267.html
  #3  
Old June 25th 08, 07:16 PM posted to rec.aviation.piloting
[email protected]
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Posts: 181
Default For the real engineers here

On Jun 25, 2:10 pm, Bertie the Bunyip wrote:
wrote in news:f21210b7-96ff-44c6-9b4b-120e489e7682@
59g2000hsb.googlegroups.com:



I'm thinking of a clean glider, one that might weigh 1500 pounds and
has a glide angle of say 1 in 25. At 50 miles an hour, that would mean
in an hour's time it might descend two miles (of course scale it
reasonable numbers, I chose those for ease of calculation). That means
it's losing about 1500 * 5280 * 2, or about 16 million foot pounds of
energy an hour.


Now if I add an engine swinging an 8 foot diameter prop, maybe as a
pusher, the question is, how big an engine for cruise only? A
horsepower is 550 foot lbs a second, or about 2 million foot pounds
an hour. If all of that is correct, it suggests with a 50% efficient
prop a little 16 horsepower engine could pretty much keep this thing
at constant altitude.


It passes the reasonableness test as far as I can see. Any serious
disagreements?


For those of you who do things in metric units? I went to school a
long long time ago, and here in the US I can buy a little Briggs and
Stanton (spelling?) engine with a horsepower rating, not a kilowatt
one.


Here ya go...

http://www.usenet.com/newsgroups/rec.../msg06267.html


Yeah, that gives some comfort that the decimal point at least is in
the right place. Thanks
  #4  
Old June 25th 08, 07:18 PM posted to rec.aviation.piloting
Bertie the Bunyip[_24_]
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Posts: 2,969
Default For the real engineers here

wrote in news:b6c58e3d-f0ee-4d52-842a-
:

On Jun 25, 2:10 pm, Bertie the Bunyip wrote:
wrote in news:f21210b7-96ff-44c6-9b4b-120e489e7682@
59g2000hsb.googlegroups.com:



I'm thinking of a clean glider, one that might weigh 1500 pounds

and
has a glide angle of say 1 in 25. At 50 miles an hour, that would

mean
in an hour's time it might descend two miles (of course scale it
reasonable numbers, I chose those for ease of calculation). That

means
it's losing about 1500 * 5280 * 2, or about 16 million foot pounds

of
energy an hour.


Now if I add an engine swinging an 8 foot diameter prop, maybe as a
pusher, the question is, how big an engine for cruise only? A
horsepower is 550 foot lbs a second, or about 2 million foot

pounds
an hour. If all of that is correct, it suggests with a 50%

efficient
prop a little 16 horsepower engine could pretty much keep this

thing
at constant altitude.


It passes the reasonableness test as far as I can see. Any serious
disagreements?


For those of you who do things in metric units? I went to school a
long long time ago, and here in the US I can buy a little Briggs

and
Stanton (spelling?) engine with a horsepower rating, not a kilowatt
one.


Here ya go...

http://www.usenet.com/newsgroups/rec.../msg06267.html

Yeah, that gives some comfort that the decimal point at least is in
the right place. Thanks


BTW, your glider will need to be a good bit lighter to have anythign
more than marginal perfoemance. With that much HP you should be grossing
about 700 lbs max.



Bertie


  #5  
Old June 25th 08, 08:44 PM posted to rec.aviation.piloting
Maxwell[_2_]
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Posts: 2,043
Default For the real engineers here


wrote in message
...

Yeah, that gives some comfort that the decimal point at least is in
the right place. Thanks


You are feeding a troll.


  #6  
Old June 25th 08, 09:13 PM posted to rec.aviation.piloting
[email protected]
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Posts: 181
Default For the real engineers here

On Jun 25, 3:44 pm, "Maxwell" luv2^fly99@cox.^net wrote:
wrote in message

...



Yeah, that gives some comfort that the decimal point at least is in
the right place. Thanks


You are feeding a troll.


I asked for information and got it. A "thank you" was a suitable
response, and I do not consider it feeding a troll, but a polite reply
to a civil answer. Maybe one person's troll is something else
elsewhere.
  #7  
Old June 25th 08, 10:43 PM posted to rec.aviation.piloting,alt.religion.asatru,alt.ozdebate,alt.usenet.kooks
Maxwell[_2_]
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Posts: 2,043
Default Froggery above

In article , Maxwell says...


wrote in message
...

Yeah, that gives some comfort that the decimal point at least is in
the right place. Thanks


You are feeding a troll.


Maxine, *you* are the troll.

As everyone here realizes.

--

"Tis an ill wind that blows no minds"
  #8  
Old June 25th 08, 11:04 PM posted to rec.aviation.piloting
Maxwell[_2_]
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Posts: 2,043
Default Forged post above

You are a common liar.



  #9  
Old June 26th 08, 12:19 AM posted to rec.aviation.piloting,alt.religion.asatru,alt.ozdebate,alt.usenet.kooks
Maxwell[_2_]
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Posts: 2,043
Default Understanding nudity

Maxwell, ye tickle-brained dunce, snakes, in my heart blood warmed, that
sting my heart. Thou Judas, thrice worse than Judas, ye gurgled:

If I learn from my mistakes, I'll learn a lot today.

  #10  
Old June 26th 08, 04:51 AM posted to rec.aviation.piloting,alt.religion.asatru,alt.ozdebate,alt.usenet.kooks
Bertie the Bunyip[_25_]
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Posts: 3,735
Default For the real engineers here

"Maxwell" luv2^fly99@cox.^net wrote in news:Qex8k.4702$i55.1320
@newsfe22.lga:


wrote in message
...

Yeah, that gives some comfort that the decimal point at least is in
the right place. Thanks


You are feeding a troll.



You are choking on your own stupidity.



Excellent.


Bertie
 




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