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48-402: H33 may refer to: H-33 (Michigan county highway) Bell H-33 , an experimental American tiltrotor aircraft Hanriot H.33 , a French biplane Highway H33 (Ukraine) HMS  H33 , a Royal Navy H-class submarine HMS  Vanoc  (H33) , a Royal Navy V-class destroyer Retinal detachment [REDACTED] Topics referred to by

96-437: 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

144-464: A feasible front line fighter by European standards, and so North American began development of a new aircraft. The British government chose a NACA-developed airfoil for the fighter, which enabled it to perform dramatically better than previous models. This aircraft became known as the P-51 Mustang . After early experiments by Opel RAK with rocket propulsion leading to the first public flight of

192-433: A nation as well as military necessity that this challenge ( Sputnik ) be met by an energetic program of research and development for the conquest of space. ... It is accordingly proposed that the scientific research be the responsibility of a national civilian agency working in close cooperation with the applied research and development groups required for weapon systems development by the military. The pattern to be followed

240-476: A result of the wind tunnel testing, the rotor diameter was reduced, wing structure was increased and strengthened, and the rotor controls were stiffened. The XV-3 resumed flight testing at Bell's facility on 12 December 1958. On 18 December 1958, Bell test pilot Bill Quinlan accomplished the first dynamically stable full conversion to airplane mode, and on 6 January 1959, Air Force Captain Robert Ferry became

288-629: A rocket plane, the Opel RAK.1 , in 1929 and eventual military programs at Heinkel and Messerschmitt by Nazi Germany in the 1930s and 1940s, the US entered the race to supersonic planes and spaceflight in the 1940s. 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

336-898: A two-year restoration, the XV-3 was transferred to the National Museum of the United States Air Force in Dayton, Ohio . It was placed on display in the museum's Post-Cold War Gallery in June 2007, and as of 2011 is on display in the Research & Development Gallery. Data from NASA Monograph 17 and Aerophile, Vol. 2, No. 1. General characteristics Performance Related development Related lists National Advisory Committee for Aeronautics The National Advisory Committee for Aeronautics ( NACA )

384-435: Is different from Wikidata All article disambiguation pages All disambiguation pages Bell H-33 The XV-3 was first flown on 11 August 1955. The first prototype use three blade rotors, and had issue with flutter crashing two months after its first flight. Tests were conducted on the second prototype with 2-blade rotors and flew successfully. Although it was limited in performance compared to later types,

432-552: Is now used in designing all transonic and supersonic aircraft. NACA experience provided a 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. On November 21, 1957, Hugh Dryden , NACA's director, established

480-576: Is that already developed by the NACA and the military services. ... The NACA is capable, by rapid extension and expansion of its effort, of providing leadership in space technology. On March 5, 1958, James Killian , who chaired the President's Science Advisory Committee , wrote a memorandum to the President Dwight D. Eisenhower . Titled, "Organization for Civil Space Programs", it encouraged

528-549: The Boeing B-17 Flying Fortress to maintain power at high altitude, a team of engineers from NACA solved the problems and created the standards and testing methods used to produce effective superchargers in the future. This enabled the B-17 to be used as a key aircraft in the war effort. The designs and information gained from NACA research on the B-17 were used in nearly every major U.S. military powerplant of

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576-573: The Convair F-102 project and the F11F Tiger . 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

624-564: The US Army's Ballistic Missile Agency would have a Jupiter C rocket ready to launch a satellite in 1956, only to have it delayed, and the Soviets would launch Sputnik 1 in October 1957. On January 14, 1958, Dryden published "A National Research Program for Space Technology", which stated: It is of great urgency and importance to our country both from consideration of our prestige as

672-610: 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,

720-643: The Naval Appropriations Bill. According to one source, "The enabling legislation for the NACA slipped through almost unnoticed as a rider attached to the Naval Appropriation Bill, on March 3, 1915." 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

768-744: The P-38 Lightning. 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

816-472: The President to sanction the creation of NASA. He wrote that a civil space program should be based on a "strengthened and redesignated" NACA, indicating that NACA was a "going Federal research agency" with 7,500 employees and $ 300 million worth of facilities, which could expand its research program "with a minimum of delay". As of their meeting on May 26, 1958, committee members, starting clockwise from

864-467: The Request for Proposals (RFP) to solicit designs from the aircraft industry. In October 1953, Bell Helicopter was awarded a development contract to produce two aircraft for testing purposes. The original military designation was XH-33 , classifying it as a helicopter , but its designation was changed to XV-3 in the convertiplane series. The designation was changed once again in 1962 to XV-3A when

912-575: 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. The offered P-40 Tomahawk fighters were considered too outdated to be

960-658: The Special Committee on Space Technology. 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. Wernher von Braun , technical director at

1008-528: The V-prefix was changed to mean VTOL . The leading designers were Bob Lichten and Kenneth Wernicke . The first XV-3 (serial number 54-147 ) flew on 11 August 1955 with Bell Chief Test Pilot Floyd Carlson at the controls. On 18 August 1955, the aircraft experienced a hard landing when the rotor developed dynamic instability. Bell attempted to remedy the situation, and flight testing resumed on 29 March 1956 after additional ground runs. Bell continued to expand

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1056-617: The XV-15 visit to Fort Rucker , Alabama, as part of a demonstration tour. 54-148 was repaired by December 1986, with Army support and the leadership of former Bell XV-3 engineer Claude Leibensberger, but the aircraft was disassembled and placed into indoor storage. On 22 January 2004, the XV-3 was delivered to Bell Plant 6 in Arlington, Texas. In 2005, Bell Helicopter employees began work to restore 54-148 to museum display condition, this time led by former XV-3 engineer Charles Davis. Following

1104-501: The XV-3 program data explaining the tiltrotor aircraft pylon whirl instability. In order to establish Hall's findings and develop a computer model, NASA agreed to conduct wind tunnel testing at the Ames 40 × 80 wind tunnel. As the engineers were completing the last planned test, a wingtip failure caused both rotors to fail, resulting in severe damage of the XV-3 and damage to the wind tunnel. On 14 June 1966, NASA Ames Research Center announced

1152-471: The aircraft had expanded the flight envelope to 127 miles per hour (204 km/h) as well as demonstrating full autorotation landings and 30-degrees forward transitions with the rotor pylons. On 6 May 1958, another instance of rotor instability occurred when the pylons were advanced to 40-degrees forward pylon angle, and the XV-3 was grounded once more. The XV-3 returned to the Ames wind tunnel in October 1958 to collect more data before it could be flown again. As

1200-463: The aircraft successfully demonstrated the tiltrotor concept, accomplishing 110 transitions from helicopter to airplane mode between December 1958 and July 1962. The XV-3 program ended when the remaining aircraft was severely damaged in a wind tunnel accident on 20 May 1966. The data and experience from the XV-3 program were key elements used to successfully develop the Bell XV-15 , which later paved

1248-406: 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's compressibility division. Compressibility is a major issue as aircraft approach Mach 1, and research into solving the problem drew heavily on information collected during previous NACA wind tunnel testing to assist Lockheed with

1296-617: 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. As the F-11F was the first design to incorporate this during initial design, it was able to break the sound barrier without having to use afterburner. Because the area rule was initially classified, it took several years for Whitcomb to be recognized for his accomplishment. In 1955 he

1344-575: The completion of XV-3 testing. The XV-3 had accomplished a total of 250 flights, accumulated 125 flight hours, and completed 110 full conversions. In late 1966, the sole remaining XV-3, serial number 54-148 , was moved to outside storage at Davis–Monthan Air Force Base in Tucson, Arizona. In 1984, the Bell XV-15 flight test team discovered the aircraft stored outside the Army's Aviation Museum during

1392-412: The deficiencies of the design, the "fixed-wing tilt-prop," or tiltrotor, was a practical application for rotorcraft. Following the completion of the joint service testing, the aircraft was returned to the Ames facility, where on 12 August 1959, Fred Drinkwater became the first NASA test pilot to complete the full conversion of a tiltrotor to airplane mode. On 8 August 1961, Army Major E. E. Kluever became

1440-399: 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

1488-449: The first Army pilot to fly a tiltrotor aircraft. Testing would continue through July 1962 as NASA and Bell completed wind tunnel testing to study pitch-flap coupling exhibited by the tiltrotor in an effort to predict and eliminate the aeroelastic dynamic rotor instability (referred to simply as pylon whirl ) that had caused problems throughout the program. In April 1966, Bell Helicopter aerodynamicist Dr. Earl Hall published an analysis of

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1536-476: The first military pilot to complete a tiltrotor conversion to airplane mode. Flight testing at the Bell facilities was completed on 24 April 1959, and the aircraft was shipped to Edwards Air Force Base. The military flight testing of the XV-3 began on 14 May 1959. Promoted to the rank of Major, Robert Ferry would coauthor the report on the military flight evaluations, conducted from May to July 1959, noting that despite

1584-399: The flight envelope of the XV-3, but on 25 July 1956, the same rotor instability occurred again. Flight testing of the XV-3 resumed in late September 1956. Then, on 25 October 1956, the aircraft crashed when the test pilot blacked out due to extremely high cockpit vibrations. The vibrations resulted when the rotor shafts were moved 17 degrees forward from vertical. The test pilot, Dick Stansbury,

1632-574: The laminar wing profiles for the North American P-51 Mustang . NACA also helped in developing the area rule that is used on all modern supersonic aircraft , and conducted the key compressibility research that enabled the Bell X-1 to break the sound barrier. NACA was established on March 13, 1915, by the federal government through enabling legislation as an emergency measure during World War I to promote industry, academic, and government coordination on war-related projects. It

1680-491: The legislation was defeated. 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

1728-463: 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. 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

1776-710: 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 . The full-size 30-by-60-foot (9.1 m × 18.3 m) Langley wind tunnel operated at no more than 100 mph (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 mph (220 kn; 400 km/h). These were speeds Lockheed engineers considered useless for their purposes. General Henry H. Arnold took up

1824-474: 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 suggested the tactic of adding the resolution to

1872-448: The same term This disambiguation page lists articles associated with the same title formed as a letter–number combination. If an internal link led you here, you may wish to change the link to point directly to the intended article. Retrieved from " https://en.wikipedia.org/w/index.php?title=H33&oldid=1085876197 " Category : Letter–number combination disambiguation pages Hidden categories: Short description

1920-564: The way for the V-22 Osprey . The remaining prototype survived to the 21st century when it was restored by Bell, with a two-year restoration that included engineers that worked on the XV-3 originally. It was then transferred to the National Museum of the United States Air Force in Dayton, Ohio , where it was put on display. In 1951, the Army and Air Force announced the Convertible Aircraft Program and released

1968-545: Was NASA during the early years after being established). 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

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2016-401: Was a United States federal agency that was 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 were transferred to the newly created National Aeronautics and Space Administration (NASA). NACA is an initialism, i.e., pronounced as individual letters, rather than as a whole word (as

2064-697: Was awarded the Collier Trophy for his work on both the Tiger and the F-102. The most important design resulting from the area rule was the B-58 Hustler , which was already in development at the time. It was redesigned to take the area rule into effect, allowing greatly improved performance. 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. The area rule concept

2112-450: 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. ... " On January 29, 1920, President Wilson appointed pioneering flier and aviation engineer Orville Wright to NACA's board. By

2160-935: Was modeled on similar national agencies found in Europe: 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 (replaced in 1918 with the Central Aerohydrodynamic Institute (TsAGI) , which is still in existence). The most influential agency upon which

2208-430: 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. In the years immediately preceding World War II, NACA was involved in the development of several designs that served key roles in the war effort. When engineers at a major engine manufacturer were having issues producing superchargers that would allow

2256-514: 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. In 1951, NACA Engineer Richard Whitcomb determined the area rule that explained transonic flow over an aircraft. The first uses of this theory were on

2304-551: Was seriously injured, and the aircraft was damaged beyond repair. Bell modified the second XV-3 (serial number 54-148 ) by replacing the three-bladed rotors with two-bladed rotors, and after taking extensive precautions, the second XV-3 began testing at the National Advisory Committee for Aeronautics ' (NACA) Ames Aeronautical Laboratory wind tunnel facility on 18 July 1957. Flight testing for aircraft #2 began on 21 January 1958 at Bell's facility. By April,

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