ArticleslgStudy

engineering

NACA cowling

NACA cowling is a engineering topic covered in the lgStudy science library. This page brings together a partial reference excerpt, illustrations, worked examples, real-world applications and a short study plan, so you can understand NACA cowling rather than just read about it. In short: The NACA cowling is a type of aerodynamic fairing used to streamline radial engines installed on airplanes. It was developed by Fred Weick of the National Advisory Committee for Aeronautics (NACA) in 1927.

NACA cowling — main illustration
NACA cowling — illustration

Key takeaways

  • NACA cowling belongs to engineering; place it in that map before memorising details.
  • Learn the definition first, then one example that makes the definition concrete.
  • Connect NACA cowling to a quantity you can measure, compute or draw — that is where exam questions come from.
  • Reproduce the core statement of NACA cowling from memory before moving on to harder problems.

Reference excerpt

The NACA cowling is a type of aerodynamic fairing used to streamline radial engines installed on airplanes. It was developed by Fred Weick of the National Advisory Committee for Aeronautics (NACA) in 1927. It was a major advancement in aerodynamic drag reduction, and paid for its development and installation costs many times over due to the gains in fuel efficiency that it enabled. NACA won the 1929 Collier Trophy for its development.

History and design

The NACA cowling enhanced speed through drag reduction while improving both engine cooling and fuel consumption. The cowling consists of a symmetric, circular airfoil that is wrapped around the engine. In a normal planar airfoil, like a wing, the difference in airspeeds, and their associated changes in pressure, on the top and bottom surfaces, enhances lift. In the case of the NACA cowl, the ring-shaped airfoil is positioned so this lift effect is forward. This thrust does not fully counter the drag of the cowl but greatly mitigates it. The difference in airspeed on the two sides is due not only to the shape of the airfoil, but also the presence of the cylinders on the inside surface, which serves to further slow the airflow. Nevertheless, the total airflow through the cowl is generally greater than it would be with no cowl as the air is sucked through the cowl by the air flowing around it. This has the side-effect of keeping the fast moving air primarily on the cylinder heads where it is most needed, as opposed to flowing between the cylinders and crankcase where it does little for cooling. Furthermore, turbulence after the air passes the free-standing cylinders is greatly reduced. The sum of all these effects reduces drag by as much as 60%. The test conclusions resulted in almost every radial-engined aircraft being equipped with this cowling, starting in 1932.

The test aircraft, a Curtiss AT-5A Hawk biplane, featuring a Wright Whirlwind J-5 radial engine, reached an airspeed of 137 miles per hour (220 km/h) equipped with the NACA cowling compared to 118 miles per hour (190 km/h) without it. Thomas Carroll tested the engine cowling as chief test pilot at Langley in 1929. The idea that the NACA cowling produced thrust through the Meredith effect is fallacious—although in theory the expansion of the air as it was heated by the engine could create some thrust by exiting at high speed, in practice this required a cowling designed and shaped to achieve the high-speed exit of air required (which the NACA cowling was not), and in any case, at 1930s airspeeds, the effect was negligible.

See also NACA airfoil NACA duct Townend ring

References

Other source Aeronautic exhibit in Smithsonian Institution, Washington, D.C.

External links

Abstract of NACA TN 301 report and .pdf file Archive of NACA reports 1917-1958

Illustrations

NACA cowling: Curtiss AT-5A Hawk with NACA cowling at the Langley Memorial Aeronautical Laboratory, October 1928
Curtiss AT-5A Hawk with NACA cowling at the Langley Memorial Aeronautical Laboratory, October 1928
NACA cowling: Close-up of the cowling on the Curtiss AT-5A[1]
Close-up of the cowling on the Curtiss AT-5A[1]
NACA cowling: "Cowling No. 10" in the Propeller Research Tunnel at the Langley Memorial Aeronautical Laboratory at Langley Field, Virginia, ca. September 1928. It became the NACA cowling.
"Cowling No. 10" in the Propeller Research Tunnel at the Langley Memorial Aeronautical Laboratory at Langley Field, Virginia, ca. September 1928. It became the NACA cowling.
NACA cowling: President Herbert Hoover presents the 1929 Collier Trophy to Dr. Joseph S. Ames of the National Advisory Committee for Aeronautics for NACA's development of the NACA cowling in a ceremony on the grounds of the White House in Washington, D.C., on 3 June 1930.
President Herbert Hoover presents the 1929 Collier Trophy to Dr. Joseph S. Ames of the National Advisory Committee for Aeronautics for NACA's development of the NACA cowling in a ceremony on the grounds of the White House in Washington, D.C., on 3 June 1930.

Worked examples

Example 1 — a first encounter with NACA cowling

Start with the simplest possible case. Write down what NACA cowling claims or describes in one sentence, then invent the smallest concrete situation in which that sentence is true. In engineering, the smallest case is usually a single object, a single equation or a single measurement. Check that every symbol or term in your sentence has a meaning in that case.

Example 2 — changing one variable

Take the situation from Example 1 and change exactly one quantity: double it, halve it, or set it to zero. Predict what should happen to NACA cowling before you calculate. Comparing your prediction with the result is the fastest way to find out whether you understand the idea or only the words.

Example 3 — an exam-style question

Typical questions about NACA cowling ask you to (a) state it precisely, (b) apply it to given data, and (c) explain a limitation. Practise writing all three answers in under five minutes; the third part is what separates a full-mark answer from an average one.

Applications of NACA cowling

In research
NACA cowling appears in engineering research whenever the underlying quantities have to be modelled precisely. Papers usually cite it as a starting assumption and then explore where it breaks down.
In technology and industry
Engineering practice reuses NACA cowling in design rules, simulations and safety margins. Knowing the idea lets you read a specification sheet and understand why the numbers look the way they do.
In the classroom
NACA cowling is common in secondary-school and first-year university syllabi. It links to neighbouring topics Aircraft aerodynamics, Aircraft components, National Advisory Committee for Aeronautics, so understanding it makes those chapters shorter.
In everyday life
Look for NACA cowling outside the textbook — in sport, cooking, traffic, electronics or the sky above you. An example you found yourself is remembered far longer than one you were given.
Ask Teacher Smith questions about this articleOpens your AI tutor with a question about “NACA cowling” →

Affiliate

Preply — study more efficiently by working with a personal tutor. 50% off.

How to study NACA cowling in 20 minutes

  1. Read the reference excerpt below once, without taking notes.
  2. Close the page and write down what NACA cowling means in your own words.
  3. Compare your version with the excerpt and mark what you missed.
  4. Work through the three examples above with pen and paper.
  5. Explain NACA cowling out loud to somebody else — or to Teacher Smith in the lgStudy chat.

Frequently asked questions

What is NACA cowling in simple terms?

The NACA cowling is a type of aerodynamic fairing used to streamline radial engines installed on airplanes. It was developed by Fred Weick of the National Advisory Committee for Aeronautics (NACA) in 1927.

Why does NACA cowling matter?

Because it connects several engineering ideas at once: it gives you a definition you can apply, a quantity you can calculate, and a way to check whether a result is plausible.

How should I study NACA cowling?

Read the excerpt, restate it from memory, then work through the examples and applications listed on this page. The five-step study plan above takes about twenty minutes.

What does this page cover?

It gives you a compact reference excerpt plus original lgStudy explanations, examples, applications and study material on NACA cowling.

Tags

  • Aircraft aerodynamics
  • Aircraft components
  • National Advisory Committee for Aeronautics

Keep exploring