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It’s all about the blades

By Jamie Beckett · June 10, 2025 · 7 Comments

A J-3 Cub taxiing. (Photo by Bidgee via Wikimedia)

Years ago, while visiting an air museum, I overheard a conversation that has stuck with me.

This particular facility employed several friends. I was a regular visitor there, an occasional helper, and a forever fan of the collection.

A man on the ramp was gazing at a P-51 Mustang as he mused aloud within earshot of an employee, “I wonder why this one has four propeller blades but that one (an L-4, the military version of the J-3 Cub) only has two.”

The employee was a good friend and an absolute whiz of an engineer. He knows more about the inner workings of flying machines than I could ever cram into my head. He’s also a remarkably kind and patient man.

“The extra blades are necessary to transfer the horsepower of the engine into the air,” offered my friend. “More power, more blades.”

You can see the four-bladed propellers on these Mustangs. (Photo by Sparky Barnes)

The visitor thought about that insight for a moment. He scratched his chin, tousled his hair, and ran little circles in the air with his index finger as he considered this newfound information. Then he spoke. “Nah, that can’t be it.”

Propellers are a mystery to most. Even to pilots they are little more than an afterthought. They seem simple enough. They are little more than a fixed form attached to a spinning shaft that produces thrust when run up to enough RPMs.

Even during the pre-flight inspection many pilots put no more thought into the propeller than to assure themselves it is indeed attached to the aircraft.

How it works, why it works, and what can be done to make it work more efficiently rarely comes up in conversation.

Well, let’s address some of those considerations.

My friend with the bright engineering mind was exactly right. The blades of a propeller are in many ways similar to the vertical stabilizer mounted to that same airplane. Surface area matters.

The Lockheed Constellation has a triple tail for the specific reason that a large surface area was needed to provide directional control for that beautiful piece of flying art deco machinery. The vertical could have been a traditional single tail, but it would have been huge. Too large to fit into most hangars of the day. But split that square footage into three parts and the overall height of the tail becomes quite manageable.

Tail of a Lockheed C-121A Constellation. (Photo by K.D. Leperi)

The same is true for propellers. The J-3 only needs two relatively short blades because that’s all physics requires to transfer the might of a 65-horsepower engine into the air.

The P-51, on the other hand, can produce as much as 1,500 hp or more. Those same two minuscule blades just aren’t going to get the job done. So the Mustangs propeller sports twice as many, longer, wider, adjustable pitch blades in an effort to get as much of that Merlin power transferred into the air as possible.

It may surprise many to know that the minimum number of blades required for a propeller to produce useable thrust is one. Few of us have ever seen such a contraption, but they do indeed exist.

They were developed by the Everel Propeller Corporation and commercially available in the 1930s. Yet, they never caught on in large numbers. But they’re out there, whirling around on the nose of some small displacement engine and proving the point that one can do it.

On the other end of the spectrum are the eight, eight-bladed, contra-rotating, constant speed propellers of the AN-22, each one measuring in at nearly 20 feet in diameter. Complex? Yes. But how else could one put as much as 15,000 shaft horsepower into the air?

The J-3’s two fixed pitch blades of roughly six feet in length just aren’t going to do it.

A front view of the AN-22. (Photo by Ministry of Defense of Russia)

The Wright brothers hand carved their two wooden propellers. They did a good job of it. Their work was surprisingly efficient and practical considering the state of the industry and the technology of their day.

Today we benefit from more than a century of experimentation in aeronautical propulsion. The simple two-bladed fixed pitch propeller is still a common sight at airports across the land. But there are new ideas on the horizon that might just change our perception of that all-important fixture pulling or pushing our aircraft forward.

Over the years we’ve seen some peculiar shapes show up. From elliptical and tapered tips, to curved trailing edges, and big squared off paddles. And let’s not forget Q-tips and scimitar blades. There are so many options you could write a book about them. In fact, people have done just that.

The floating gas bag gave rise to the airplane. The airplane led to experimentation and the eventual development of the helicopter. New, mission specific aircraft have been in development since the Montgolfier brothers first sent a collection of livestock skyward in a hot air balloon in the late 1700s. All of it struck the public as fascinating, a bit scary, but largely useless — until they realized it was in fact absolutely life altering.

The pace of change continues. Today, drones are making headway into our daily lives, which has led to even more unique propeller design ideas coming to the fore. Yes, I speak of the toroidal propeller.

A 3-blade toroidal propeller. (Photo by Sauer202 via Wikipedia)

A peculiar looking sci-fi inspired device with blades that loop back on themselves to rejoin at the hub. These propellers can be roughly as efficient in terms of lift as a traditional two-bladed design. Their benefits aren’t found in the realm of thrust, however. It is in their ability to produce thrust very, very quietly.

Might aircraft of the future be quiet, efficient, beautiful, and practical? Yes, I believe they will be, even more than they are today. But I will always have a soft spot in my heart for the Constellation and the J-3.

The classics have their place even as we set our sights on the moon and Mars. Efficiency isn’t everything.

About Jamie Beckett

Jamie Beckett is the AOPA Foundation’s High School Aero Club Liaison. A dedicated aviation advocate, you can reach him at: [email protected]

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Comments

  1. Terk Williams says

    June 11, 2025 at 9:14 am

    Nice piece Jamie. I taught and when we went “digital” at ECAT (East Coast Aero Tech, 147 A&P school) I had the chance to “ modernize” the props class. I was also privy to the faa red tagging the twin w the early “Q” tip props LOL. They were certain it was a gear up prop strike…Two of the useful things for pilots to ponder are 1) the tip speed of a 96” prop at 2,700 rpm.. no free ride. Do the math 😎. Think “noise” of this highly efficient long, thin float plane prop. Why so loud? (A clue: think sound barrier..)…Second is to appreciate the different pitches of the blade from root to tip relative to its speed through the air and angle if attack at a given “station” ( measured center hub, usually in inches in this country. At some defined station (typically @ 3/4 span..) provides the second number on a fixed pitch. First being length, tip to tip, second the distance that station would theoretically travel in still air) out to tip, like on your wt n bal). The inboard portion is actually turning quite slowly so wants a “fat” (high lift) airfoil vs the much lower pitch, thin blade near the higher velocity at the tip. This all yields equal thrust from all stations 😎. Oh, and the terminology, the ‘face’ is the ‘flat’ side that faces the pilot in a tractor (pulling vs pushing) prop. The ‘humpy, back’ is just that, the back. I didn’t name ‘em, I just convey the lesson.

    A bit of run on, Sorry. In haste but had to jump in.

    Reply
    • Jamie Beckett says

      June 11, 2025 at 11:07 am

      Excellent insight, Terk. Thanks for sharing.

      Reply
  2. JimH in CA says

    June 10, 2025 at 9:47 pm

    Janie,

    I missed your last comment on the tail.
    Sorry for my misreading/ miss-understanding…!!!

    Reply
    • JimH in CA says

      June 10, 2025 at 9:52 pm

      Jamie,
      And I can’t type well either…part of the ‘old man’ syndrome.

      Reply
  3. JimH in CA says

    June 10, 2025 at 11:06 am

    Nice article on props, but the reference to the Connie triple tail was not correct;
    ‘…The Constellation had a triple tail design to help it fit into hangars made for smaller aircraft, like the DC-3. ‘

    Reply
    • Jamie Beckett says

      June 10, 2025 at 5:32 pm

      I’m just curious, JimH. How does your assertion that the Connie tail was designed to fit into traditional hangars differ from mine that the Connie tail was designed to fit into traditional hangars. The nuance is lost on me.

      Reply
      • JimH in CA says

        June 10, 2025 at 9:37 pm

        Jamie,

        a google search turned up a number of references;
        ie, https://simpleflying.com/why-lockheed-constellation-had-three-tails/

        A single tail would be too tall to fit, since it was very tall on the gear.

        I wasn’t being critical just some minor correction…
        I really like this site where we can discuss the articles and hopefully learn something that would learn how to not get into the situation.

        regards, JimH. N8234T

        Reply

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