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National Advisory Committee for Aeronautics

National Advisory Committee for Aeronautics
The official seal of NACA, depicting the Wright brothers' first flight at Kitty Hawk, North Carolina
Agency overview
Formed March 3, 1915
Dissolved October 1, 1958
Superseding agency
Jurisdiction Federal government of the United States

The National Advisory Committee for Aeronautics (NACA) was a U.S. federal agency founded on March 3, 1915, to undertake, promote, and institutionalize aeronautical research. On October 1, 1958, the agency was dissolved, and its assets and personnel transferred to the newly created National Aeronautics and Space Administration (NASA). NACA was pronounced as individual letters, rather than as an acronym[1] (and after NASA first came into being, it too was vocalized as individual letters as well).[2]

Among other advancements, NACA research and development produced the NACA duct, a type of air intake used in modern automotive applications, the NACA cowling, and several series of NACA airfoils which are still used in aircraft manufacturing.

During World War II, NACA was described as "The Force Behind Our Air Supremacy" due to its key role in producing working superchargers for high altitude bombers, and for producing the cutting edge wing profiles for the North American P-51 Mustang.[3] NACA was also key in developing the area rule that is used on all modern supersonic aircraft, and was responsible for the key compressibility research that allowed the Bell X-1 to break the sound barrier.


  • Origins 1
  • Research at NACA 2
  • Influence on technology immediately before and during World War II 3
  • NACA involvement in supersonic research 4
  • Special Committee on Space Technology 5
  • Transformation into NASA 6
  • NASA Advisory Council 7
  • NACA wind tunnels 8
  • NACA chairmen 9
  • Members of Special Committee on Space Technology 10
  • Footnotes and references 11
  • Further reading 12
  • External links 13


The inscription on the wall is NACA's mission statement: "...It shall be the duty of the advisory committee for aeronautics to supervise and direct the scientific study of the problems of flight with a view to their practical solution..." By an Act of Congress Approved March 3, 1915

NACA began as an emergency measure during World War I to promote industry/academic/government coordination on war-related projects. It was modeled on similar national agencies found in Europe. Such agencies were the French L’Etablissement Central de l’Aérostation Militaire in Meudon (now Office National d'Etudes et de Recherches Aerospatiales), the German Aerodynamic Laboratory of the University of Göttingen, and the Russian Aerodynamic Institute of Koutchino with a Soviet successor agency, the "Central Aerohydrodynamic Institute", still known in post-Soviet Russia as TsAGI today, in 1918. However, the most influential agency upon which the NACA was based was the British Advisory Committee for Aeronautics.

In December 1912, President William Howard Taft had appointed a National Aerodynamical Laboratory Commission chaired by Robert S. Woodward, president of the Carnegie Institution of Washington. Legislation was introduced in both houses of Congress early in January 1913 to approve the commission, but when it came to a vote, the legislation was defeated.

The first meeting of the NACA in 1915

Charles D. Walcott – secretary of the Smithsonian Institution from 1907 to 1927 – took up the effort, and in January 1915, Senator Benjamin R. Tillman, and Representative Ernest W. Roberts introduced identical resolutions recommending the creation of an advisory committee as outlined by Walcott. The purpose of the committee was "to supervise and direct the scientific study of the problems of flight with a view to their practical solution, and to determine the problems which should be experimentally attacked and to discuss their solution and their application to practical questions." Assistant Secretary of the Navy Franklin D. Roosevelt wrote that he "heartily [endorsed] the principle" on which the legislation was based. Walcott then suggested the tactic of adding the resolution to the Naval Appropriations Bill.[4]

According to one source, "The enabling legislation for the NACA slipped through almost unnoticed as a rider attached to the Naval Appropriation Bill, on 3 March 1915."[5] The committee of 12 people, all unpaid, were allocated a budget of $5,000 per year.

President Woodrow Wilson signed it into law the same day, thus formally creating the Advisory Committee for Aeronautics, as it was called in the legislation, on the last day of the 63rd Congress.

The act of Congress creating NACA, approved March 3, 1915, reads, "...It shall be the duty of the advisory committee for aeronautics to supervise and direct the scientific study of the problems of flight with a view to their practical solution...."[6]

Research at NACA

The NACA Test Force at the High-Speed Flight Station in Edwards, California. The white aircraft in the foreground is a Douglas Skyrocket.

On January 29, 1920, President Wilson appointed pioneering flier and aviation engineer Orville Wright to NACA's board. By the early 1920s, it had adopted a new and more ambitious mission: to promote military and civilian aviation through applied research that looked beyond current needs. NACA researchers pursued this mission through the agency's impressive collection of in-house wind tunnels, engine test stands, and flight test facilities. Commercial and military clients were also permitted to use NACA facilities on a contract basis.


In 1922, NACA had 100 employees. By 1938, it had 426. In addition to formal assignments, staff were encouraged to pursue unauthorized "bootleg" research, provided that it was not too exotic. The result was a long string of fundamental breakthroughs, including "thin airfoil theory" (1920s), "NACA engine cowl" (1930s), the "NACA airfoil" series (1940s), and the "area rule" for supersonic aircraft (1950s). On the other hand, NACA's 1941 refusal to increase airspeed in their wind tunnels set Lockheed back a year in their quest to solve the problem of compressibility encountered in high speed dives made by the Lockheed P-38 Lightning.[7]

An engineer makes final calibrations to a model mounted in the 6-by-6-foot (1.8 m × 1.8 m) supersonic wind tunnel.

The full-size 30-by-60-foot (9.1 m × 18.3 m) Langley wind tunnel operated at no more than 100 miles per hour (87 kn; 160 km/h) and the then-recent 7-by-10-foot (2.1 m × 3.0 m) tunnels at Moffett could only reach 250 miles per hour (220 kn; 400 km/h). These were speeds Lockheed engineers considered useless for their purposes. General Henry H. Arnold took up the matter and overruled NACA objections to higher air speeds. NACA built a handful of new high-speed wind tunnels, and Mach 0.75 (570 mph (495 kn; 917 km/h) was reached at Moffett's 16-foot (4.9 m) wind tunnel late in 1942.[8][9]

Influence on technology immediately before and during World War II

In the years immediately preceding World War II, NACA was involved in several designs that went on to serve key roles in the war effort. When engineers at a major engine manufacturer were having issues producing superchargers that would allow the Boeing B-17 Flying Fortress to maintain power at high altitude, it was a team of engineers from NACA who solved the problems and who created the standards and testing methods used to produce effective superchargers in the future. This allowed the B-17 to become a key aircraft in the war effort. The designs and information gained from NACA research on the B-17 were utilized in nearly every major U.S. military powerplant of the Second World War. Nearly every aircraft used some form of forced induction that relied on information developed by NACA. Because of this, U.S. produced aircraft had a significant power advantage above 15,000 feet, which was never fully countered by Axis forces.

After the war had begun, the British government sent a request to North American Aviation for a new fighter. Their existing P-40 fighter was considered too outdated to be a feasible front line fighter, and so the development of a new aircraft was begun. A NACA developed airfoil was chosen by the British government for the fighter, which allowed it to perform dramatically better than previous models. The aircraft became the P-51 Mustang.[10]

NACA involvement in supersonic research

The NACA XS-1 (Bell X-1)

Although the Bell X-1 was commissioned by the Air Force and flown by Air Force test pilot Chuck Yeager, when it exceeded Mach 1 NACA was officially in charge of the testing and development of the aircraft. NACA ran the experiments and data collection, and the bulk of the research used to develop the aircraft came from NACA engineer John Stack, the head of NACA compressibility division. [11] Compressibility is a major issue as aircraft approach Mach 1, and research into solving the problem drew heavily on information collected from Lockheed engineers solving the P-38's dive difficulties.

The X-1 program was first envisioned in 1944 when a former NACA engineer working for Bell Aircraft approached the Army for funding of a supersonic test aircraft. Neither the Army nor Bell had any experience in this area, so the majority of research came from the NACA Compressibility Research Division, which had been operating for more than a year by the time Bell began conceptual designs. The Compressibility Research Division also had years of additional research and data to pull from, as its head engineer was previously head of the high speed wind tunnel division, which itself had nearly a decade of high speed test data by that time. Due to the importance of NACA involvement, Stack was personally awarded the Collier Trophy along with the owner of Bell Aircraft and test pilot Chuck Yeager.[12][13]

The NACA Scientific and Engineering Staff at the Ames Research Center in Mountain View California shortly before the dissolution of NACA and the formation of NASA in 1958.

In 1951, NACA Engineer Richard Whitcomb determined the area rule that explained transonic flow over an aircraft. The first use of this theory was on the U.S. Air Force Convair F-102 project. The F-102 was meant to be a supersonic interceptor, but it was unable to exceed the speed of sound, despite the best effort of Convair engineers. The F-102 had actually already begun production when this was discovered, so NACA engineers were sent to quickly solve the problem at hand. The production line had to be modified to allow the modification of F-102s already in production to allow them to use the area rule. (Aircraft so altered were known as "area ruled" aircraft.) The design changes allowed the aircraft to exceed Mach 1, but only by a small margin, as the rest of the Convair design was not optimized for this.[14]

The area rule was immediately adapted by Grumman to modify its F9F Cougar, an already successful naval fighter. The result was the F11F Tiger. The area rule was used to design the Vought F-8 Crusader.

The most important design resulting from the area rule was the B-58 Hustler.[15] This was the first US supersonic bomber, and was capable of Mach 2 at a time when Soviet fighters had only just attained that speed months earlier.[16] The area rule concept is now used in designing all transonic and supersonic aircraft.

NACA experience provided a powerful model for World War II research, the postwar government laboratories, and NACA's successor, the National Aeronautics and Space Administration (NASA).

NACA also participated in development of the first aircraft to fly to the "edge of space", North American's X-15. NACA airfoils are still used on modern aircraft.

Special Committee on Space Technology

Foreground: Wernher von Braun; fourth from the left, Hendrik Wade Bode. See also list below running in a clockwise direction

On 21 November 1957, Hugh Dryden, NACA’s director, established the Special Committee on Space Technology.[17] The committee, also called the Stever Committee after its chairman, Guyford Stever, was a special steering committee that was formed with the mandate to coordinate various branches of the federal government, private companies as well as universities within the United States with NACA's objectives and also harness their expertise in order to develop a space program.[18]

Wernher von Braun would have a Jupiter C rocket ready to launch a satellite in 1956, only to have it delayed,[19] and the Soviets would launch Sputnik 1 in October 1957.

Transformation into NASA

On January 14, 1958, Dryden published "A National Research Program for Space Technology," which stated:[17]

On March 5, 1958, [17]

NASA Advisory Council

With the creation of NASA in 1958, the NACA was abolished, and its research centers – Ames Research Center, Lewis Research Center, and Langley Aeronautical Laboratory – were incorporated within the new space and aeronautics agency along with some elements of the U.S. Army and U.S. Navy. In 1967, Congress directed NASA to form an Aerospace Safety Advisory Panel (ASAP) to advise the NASA Administrator on safety issues and hazards in NASA's aerospace programs. In addition, there were the Space Program Advisory Council and the Research and Technology Advisory Council.

In 1977, these were all combined to form the NASA Advisory Council (NAC) which is the successor to the National Advisory Committee for Aeronautics.[20]

NACA wind tunnels

NACA wind test on a human subject (1946)

NACA's first wind tunnel was formally dedicated at Langley Memorial Aeronautical Laboratory on June 11, 1920. It was the first of many now-famous NACA and NASA wind tunnels. Although this specific wind tunnel was not unique or advanced, it enabled NACA engineers and scientists to develop and test new and advanced concepts in aerodynamics and to improve future wind tunnel design.

  1. Atmospheric 5-ft wind tunnel (1920)
  2. Variable Density Tunnel (1922)
  3. Propeller research tunnel (1927)
  4. High-speed 11-in wind tunnel (1928)
  5. Vertical 5-ft wind tunnel (1929)
  6. Atmospheric 7- by 10-ft wind tunnel (1930)
  7. Full-scale 30- by 60-ft tunnel (1931)

NACA chairmen

  1. United States Army) (1915–1916)
  2. William F. Durand (Stanford University) (1916–1918)
  3. John R. Freeman (consultant) (1918–1919)
  4. Charles Doolittle Walcott (Smithsonian Institution) (1920–1927)
  5. Joseph Sweetman Ames (Johns Hopkins University) (1927–1939)
  6. Vannevar Bush (Carnegie Institution) (1940–1941)
  7. Jerome C. Hunsaker (Navy, MIT) (1941–1956)
  8. James H. Doolittle (Shell Oil) (1957–1958)

Members of Special Committee on Space Technology

As of their meeting on 26 May 1958, committee members, starting clockwise from the left of the above picture:[18]

Committee member Title
Edward R. Sharp Director of the Lewis Flight Propulsion Laboratory
Colonel Norman C Appold Assistant to the Deputy Commander for Weapons Systems, Air Research and Development Command: US Air Force
Abraham Hyatt Research and Analysis Officer Bureau of Aeronautics, Department of the Navy
Hendrik Wade Bode Director of Research Physical Sciences, Bell Telephone Laboratories
William Randolph Lovelace II Lovelace Foundation for Medication Education and Research
S. K Hoffman General Manager, Rocketdyne Division, North American Aviation
Milton U Clauser Director, Aeronautical Research Laboratory, The Ramo-Wooldridge Corporation
H. Julian Allen Chief, High Speed Flight Research, NACA Ames
Robert R. Gilruth Assistant Director, NACA Langley
J. R. Dempsey Manager. Convair-Astronautics (Division of General Dynamics)
Carl B. Palmer Secretary to Committee, NACA Headquarters
H. Guyford Stever Chairman, Associate Dean of Engineering, Massachusetts Institute of Technology
Hugh L. Dryden (ex officio), Director, NACA, Namesake of future Dryden Research Center
Dale R. Corson Department of Physics, Cornell University
Abe Silverstein Associate Director, NACA Lewis
Wernher von Braun Director, Development Operations Division, Army Ballistic Missile Agency

Footnotes and references

  1. ^ Murray, Charles, and Catherine Bly Cox. Apollo. South Mountain Books, 2004, p. xiii.
  2. ^ Creation of NASA: Message to Employees of NACA from T. Keith Glennan (1958 NASA film)
  3. ^
  4. ^ Roland, Alex. "Model Research - Volume 1". Archived from the original on 2004-11-13. 
  5. ^ Bilstein, Roger E. "Orders of Magnitude, Chapter 1". 
  6. ^ Dawson, Virginia P. "Engines and Innovation". Archived from the original on 2004-10-31. 
  7. ^ Bodie, Warren M. The Lockheed P-38 Lightning: The Definitive Story of Lockheed's P-38 Fighter. Hayesville, North Carolina: Widewing Publications, 2001, 1991, pp. 174–5. ISBN 0-9629359-5-6.
  8. ^ Bodie, Warren M. The Lockheed P-38 Lightning. pp. 75-6.
  9. ^ The First Big High Speed Tunnel
  10. ^
  11. ^
  12. ^ From Engineering Science to Big Science: The NACA and NASA Collier Trophy Research Project Winners, 1998, P.89
  13. ^ "Dryden Flight Research Center historical data". NASA. Retrieved 2006-12-10. 
  14. ^ From Engineering Science to Big Science: The NACA and NASA Collier Trophy Research Project Winners, 1998, p. 146.
  15. ^ From Engineering Science to Big Science: The NACA and NASA Collier Trophy Research Project Winners, 1998, P.147
  16. ^
  17. ^ a b c Erickson, Mark. Into the Unknown Together - The DOD, NASA, and Early Spaceflight (PDF).  
  18. ^ a b NASA Historical Website
  19. ^ [The Race pp18 ISBN 0-385-49253-7]
  20. ^ NASA Advisory Council

Further reading

  • Orders of Magnitude: A History of the NACA and NASA, 1915-1990John Henry, et al. .
  • Model Research: The National Advisory Committee for Aeronautics, 1915-1958.Alex Roland.
  • Engineer in Charge: A History of the Langley Aeronautical Laboratory, 1917-1958.James Hansen.
  • Expanding the envelope – Flight Research at NACA and NASA.Michael H. Gorn,

External links

  • U.S. Centennial of Flight Commission: The National Advisory Committee for Aeronautics (NACA)
  • The NASA Technical Reports Server provides access to a collection of 14,469 NACA documents dating from 1917.
  • Information on NACA airfoil series
  • "From Engineering Science to Big Science" — The NACA and NASA Collier Trophy Research Project Winners, edited by Pamela E. Mack.
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