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force generated by propeller?

Started byChristopher Howard <christopher@librehacker.com>
First post2026-01-30 12:17 -0900
Last post2026-02-02 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

#895001 — force generated by propeller?

FromChristopher Howard <christopher@librehacker.com>
Date2026-01-30 12:17 -0900
Subjectforce 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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#895005

FromJim Pennino <jimp@gonzo.specsol.net>
Date2026-01-30 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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#895031

FromChristopher Howard <christopher@librehacker.com>
Date2026-02-02 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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#895034

FromJim Pennino <jimp@gonzo.specsol.net>
Date2026-02-02 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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#895011

FromThomas 'PointedEars' Lahn <PointedEars@web.de>
Date2026-02-01 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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#895030

FromChristopher Howard <christopher@librehacker.com>
Date2026-02-02 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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