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| Started by | Christopher Howard <christopher@librehacker.com> |
|---|---|
| First post | 2026-01-30 12:17 -0900 |
| Last post | 2026-02-02 07:36 -0900 |
| Articles | 6 — 3 participants |
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force generated by propeller? Christopher Howard <christopher@librehacker.com> - 2026-01-30 12:17 -0900
Re: force generated by propeller? Jim Pennino <jimp@gonzo.specsol.net> - 2026-01-30 15:57 -0800
Re: force generated by propeller? Christopher Howard <christopher@librehacker.com> - 2026-02-02 07:44 -0900
Re: force generated by propeller? Jim Pennino <jimp@gonzo.specsol.net> - 2026-02-02 09:09 -0800
Re: force generated by propeller? Thomas 'PointedEars' Lahn <PointedEars@web.de> - 2026-02-01 06:38 +0100
Re: force generated by propeller? Christopher Howard <christopher@librehacker.com> - 2026-02-02 07:36 -0900
| From | Christopher Howard <christopher@librehacker.com> |
|---|---|
| Date | 2026-01-30 12:17 -0900 |
| Subject | force generated by propeller? |
| Message-ID | <87h5s2iyw7.fsf@librehacker.com> |
Hi, I did some reading up on the basic math for jet aircraft, thrust-to-weight ratio, and related concepts. I was trying to relate this understanding to propeller driven aircraft, like a small single-prop plane. When I see the stats for these small planes in magazines, the engine horsepower is listed, along with the power loading and empty weight. I was wondering if it was possible, without diving too deeply into the math and details, to roughly figure out the lbf that can be generated by a propeller with, say, a 100 hp engine. Maybe by making a bunch of simplifying assumptions, like a typical propeller, standard barometric pressure, and such like? -- Christopher Howard
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| From | Jim Pennino <jimp@gonzo.specsol.net> |
|---|---|
| Date | 2026-01-30 15:57 -0800 |
| Message-ID | <n4tv4m-n7r3.ln1@gonzo.specsol.net> |
| In reply to | #895001 |
Christopher Howard <christopher@librehacker.com> wrote: > Hi, I did some reading up on the basic math for jet aircraft, > thrust-to-weight ratio, and related concepts. I was trying to relate > this understanding to propeller driven aircraft, like a small > single-prop plane. When I see the stats for these small planes in > magazines, the engine horsepower is listed, along with the power loading > and empty weight. > > I was wondering if it was possible, without diving too deeply into the > math and details, to roughly figure out the lbf that can be generated by > a propeller with, say, a 100 hp engine. Maybe by making a bunch of > simplifying assumptions, like a typical propeller, standard barometric > pressure, and such like? > There is a rule of thumb that a decent propeller makes about 20 lbs thrust per 10 HP. Alternately Google "how to calculate propeller thrust". -- penninojim@yahoo.com
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| From | Christopher Howard <christopher@librehacker.com> |
|---|---|
| Date | 2026-02-02 07:44 -0900 |
| Message-ID | <87cy2ndrjh.fsf@librehacker.com> |
| In reply to | #895005 |
Jim Pennino <jimp@gonzo.specsol.net> writes:
>
> There is a rule of thumb that a decent propeller makes about 20 lbs
> thrust per 10 HP.
Okay, thank you, that is helpful to know.
>
> Alternately Google "how to calculate propeller thrust".
I don't use Google search, but DDG gives some results that are a bit
difficult to wade through. The propeller thrust calculator page gives
these equations:
Velocity = Propeller Pitch * RPM * (1/1056)
Thrust = (2 * Efficiency * Power * 746)
/ (Velocity * Propeller Diameter * 0.0254)
with the Power in watts and the pitch and diameter in inches. That
doesn't sound too complicated to calculate.
--
Christopher Howard
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| From | Jim Pennino <jimp@gonzo.specsol.net> |
|---|---|
| Date | 2026-02-02 09:09 -0800 |
| Message-ID | <hb275m-f81l.ln1@gonzo.specsol.net> |
| In reply to | #895031 |
Christopher Howard <christopher@librehacker.com> wrote: > Jim Pennino <jimp@gonzo.specsol.net> writes: >> >> There is a rule of thumb that a decent propeller makes about 20 lbs >> thrust per 10 HP. > > Okay, thank you, that is helpful to know. > >> >> Alternately Google "how to calculate propeller thrust". > > I don't use Google search, but DDG gives some results that are a bit > difficult to wade through. The propeller thrust calculator page gives > these equations: > > Velocity = Propeller Pitch * RPM * (1/1056) > > Thrust = (2 * Efficiency * Power * 746) > / (Velocity * Propeller Diameter * 0.0254) > > with the Power in watts and the pitch and diameter in inches. That > doesn't sound too complicated to calculate. > Yeah, but this too is more a rule of thumb. -- penninojim@yahoo.com
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| From | Thomas 'PointedEars' Lahn <PointedEars@web.de> |
|---|---|
| Date | 2026-02-01 06:38 +0100 |
| Message-ID | <10lmot1$l7fi$1@gwaiyur.mb-net.net> |
| In reply to | #895001 |
Christopher Howard wrote: > I was wondering if it was possible, without diving too deeply into the > math and details, to roughly figure out the lbf that can be generated by > a propeller with, What do you mean by "the lbf that can be generated"? -- PointedEars Twitter: @PointedEars2 Please do not cc me. / Bitte keine Kopien per E-Mail.
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| From | Christopher Howard <christopher@librehacker.com> |
|---|---|
| Date | 2026-02-02 07:36 -0900 |
| Message-ID | <87jywvdrwc.fsf@librehacker.com> |
| In reply to | #895011 |
Thomas 'PointedEars' Lahn <PointedEars@web.de> writes: > Christopher Howard wrote: >> I was wondering if it was possible, without diving too deeply into the >> math and details, to roughly figure out the lbf that can be generated by >> a propeller with, > > What do you mean by "the lbf that can be generated"? With the wikipedia articles on jet aircraft, there is usually listed the pounds-force thrust that is generated by each of the engines, which along with the empty weight (or whatever additional weight you want to add) can be used easily to calculate the thrust-to-weight ratio. Some fighter aircraft achieve 1:1 but most commercial jets are somewhere around 0.6 to 0.7, from what I can tell. In the specs I was seeing for propeller aircraft, it seems what is usually listed is weight-per-horsepower, or power loading. That is interesting, but I was having trouble seeing how to compare the two. Thrust is more intuitive to me one can see directly the ratio between thrust lbf and weight lbs. -- Christopher Howard
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