Jack Ridley

American Aeronautical Engineer And Test Pilot

Jack Ridley was born in Garvin, Oklahoma, United States on June 16th, 1915 and is the American Aeronautical Engineer And Test Pilot. At the age of 41, Jack Ridley biography, profession, age, height, weight, eye color, hair color, build, measurements, education, career, dating/affair, family, news updates, and networth are available.

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Date of Birth
June 16, 1915
Nationality
United States
Place of Birth
Garvin, Oklahoma, United States
Death Date
Mar 12, 1957 (age 41)
Zodiac Sign
Gemini
Profession
Aerospace Engineer, Aircraft Pilot, Engineer, Military Officer
Jack Ridley Height, Weight, Eye Color and Hair Color

At 41 years old, Jack Ridley physical status not available right now. We will update Jack Ridley 's height, weight, eye color, hair color, build, and measurements.

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Jack Ridley Religion, Education, and Hobbies
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Hobbies
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Education
University of Oklahoma, B.S. 1939, Caltech, M.S. 1945
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Jack Ridley Career

The Air Corps needed engineering-trained pilots and, instead of being sent into an operational combat unit, Ridley was ordered to the Consolidated Vultee plant in Fort Worth, Texas, where his initial assignment was to conduct acceptance tests on four-engine B-24 Liberator bombers. Soon thereafter, he was named as engineering liaison officer on both the B-24 and B-32 programs. Even at that early date, the Air Corps was developing the six-engine B-36 intercontinental bomber, later to become the mainstay of the postwar Strategic Air Command, and Ridley found himself assigned to that program as well.

In 1944, Ridley was sent off to further his education. After attending the Army Air Forces School of Engineering at Wright Field (later renamed the Air Force Institute of Technology), Ridley was sent to the California Institute of Technology, in Pasadena, California where he received his Master of Science degree in aeronautical engineering in July 1945.

Postwar career

Ridley was sent to Wright Field, Ohio, and assigned to the Air Materiel Command's Flight Test Division. Ridley went to the Air Materiel Command Flight Performance School from January through May 1946. In the spring of 1946, he graduated with Class 46A.

Even as Ridley was attending the Flight Performance School, the revolutionary X-1 rocket research airplane was making its initial unpowered check flights and, within a year, the USAAF (soon to achieve independence as the United States Air Force) would assume control of the supersonic research program. Colonel Albert Boyd, the chief of the Flight Test Division selected the project team that would attempt the world's first supersonic flight. In the spring of 1947, Boyd appraised his roster of 125 test pilots and finally selected three volunteers who were considered very junior in terms of their flight test experience: Captain Charles E. "Chuck" Yeager, 1st Lieutenant Robert A. "Bob" Hoover, and Ridley. He named Yeager and Hoover as primary and backup pilot respectively, and Ridley as project engineer.

The choice was a happy one. As Yeager later explained:

Ridley's task was to analyze all of the technical data that was generated during the X-1 flights as it proceeded toward the unexplored region of supersonic flight. Studying the phenomena that the research plane encountered as it passed through the transonic region, he translated all of the information into pilot terminology for Yeager so that the flight program could be carried forward expeditiously, yet with safety. As Yeager later explained:

Ridley had to rise to meet unexpected problems and new aerodynamic principles. He faced the problem of a complete loss of elevator effectiveness which Yeager experienced during his eighth powered flight as his Mach meter indicated a speed of Mach 0.94 (his true airspeed was in the range of 0.96-0.99 Mach, just below the speed of sound). At that speed, the little research plane stopped responding to all elevator control inputs, leaving the pilot unable to change his pitch angle, or to raise or lower the plane's nose in flight. When speed decreased slightly, the problem abruptly disappeared. Analysis suggested that a shockwave was forming along the elevator's hinge line, leaving it ineffective. Ridley determined in that speed range, the elevator itself could safely be dispensed with and the X-1's entire horizontal stabilizer, which could be adjusted for trim changes, be used for pitch control. The idea worked, and Ridley's concept eventually came to be incorporated in all supersonic aircraft — the "flying tail."

Ridley also improvised a vital piece of equipment at the last minute. Two days before taking the X-1 on its first supersonic flight, Chuck Yeager broke two ribs in a horseback riding accident. With the aid of an understanding civilian doctor, he was able to conceal his condition from everyone but Ridley. Without the full use of his right arm, however, it would be impossible to seal himself into the tiny X-1 cockpit. Ridley quietly provided a length of broom handle that Yeager was able to use to close the hatch without difficulty.

If Yeager was a superb "intuitive engineer," able to identify the cause of any unexpected event in the air, Ridley was equally gifted in his computational and reasoning abilities. Indeed, Yeager often called him "the brains behind the whole X-1 test program." All three team members meshed well together. All were pragmatic, hands-on types with an instinct to ferret out a straightforward, practical solution to each problem as soon as it arose. The result was an energetic team of young professionals who fulfilled Colonel Boyd's most exacting expectations and, on October 14, 1947, led the world into the supersonic age. The Air Force recognized his efforts three years later by awarding him the Commendation Ribbon for meritorious achievement.

Ridley worked on the X-1 project until May 1948, when he was sent to the state of Washington for temporary assignment to the XB-47 program. The swept-wing Stratojet, powered by six J-47 turbojet engines and capable of high subsonic speeds, was in its way as revolutionary as the X-1 had been. His expertise proved instrumental in bringing the revolutionary jet bomber to operational status with the Strategic Air Command. A year later, the flight test engineer was permanently assigned to Muroc Army Air Field (soon to be renamed Edwards Air Force Base) where he remained, with interruptions, until 1956.

Returning to Edwards Air Force Base, Ridley applied his reasoning skills to many of the new generation of jet and rocket aircraft then arriving on the ramp: the delta-winged XF-92A, the F-84F Thunderstreak, and the nation's new heavyweight bomber, the B-52. He worked on the entire family of Air Force research airplanes from the X-1 through the variable-sweep wing X-5. His responsibilities included planning flight test programs for various aircraft, identifying the stability characteristics and gathering the performance data which would later be used in writing Pilots Operating Handbooks and compiling standard aircraft characteristic charts.

Ridley corrected a problem with over-sensitive controls on the F-86E Sabre, which was still unsolved after several test flights. Waiting until night had fallen, Ridley led a team of engineers into a darkened hangar. There, he placed a flashlight on the horizontal tail and climbed into the cockpit. The flashlight beam, moving across the hangar door in response to his control inputs, easily revealed a lag problem, which could soon be corrected.

He never really turned off the computational portion of his mind, even when he was absorbed in other work. One evening found him deep in conversation at the officers club, planning the engineering aspects of an upcoming test series with the project pilot for the XF-91 rocket-assisted fighter program. Four master's degree hopefuls from MIT were seated at a nearby table, fretting at their inability to solve a complex problem which they had been assigned. Never breaking the thread of his own conversation, Ridley abruptly handed the students a notepad he had been scribbling on: "Would this help you any?" Cries of joy followed by hearty thumps on his back acknowledged his ingenious solution to their dilemma.

From project engineer, he was selected to be chief of the Test Engineering Branch. From this post he was subsequently promoted to Chief, Flight Test Engineering Laboratory. The responsibility of this division-level organization was to carry out the research and engineering phases of all of the experimental flight test programs assigned to the AFFTC, including overseeing such details as the human factors program and overseeing the weighing and balancing of aircraft. Ridley's new organization included separate branches for Data Reduction, Performance Engineering and Flight Research. It was in this post that he made his longest-lasting contributions to the science of flight testing.

Working with the Flight Test Center's Technical Director, Paul Bikle, he defined the basic flight test techniques that are still used by the Air Force Flight Test Center. Aiming to reduce the increasing length of time and costs required to determine the results of the center's flight tests, they standardized all of its data acquisition methods and set up a centralized Data Processing System. This made it possible for test teams to analyze their test data more rapidly, and to publish their Technical Reports more quickly. He also established training and indoctrination procedures for new military and civilian flight test engineers. Impressing his own long-thought-out ideals upon these changes and goals, Jack Ridley is still credited for creating the Flight Test Center's basic philosophy in use today.

By this point in his career, his professional reputation had already spread far afield. Dr. Theodore von Kármán, Chairman of the Advisory Group for Aeronautical Research and Development (AGARD), nominated the young lieutenant colonel to represent the United States on its Flight Test Techniques Panel. This appointment was a signal honor. AGARD, a Standing Group of the North Atlantic Treaty Organization (NATO) had been created to bring together the leading aeronautical experts from each of the member nations to find ways to use aviation research and development personnel and facilities for the common benefit of the member nations. Ridley served in this prestigious position from 1952 until 1956.

Ridley was promoted to full colonel in 1956 and became a member of the U.S. Military Assistance Advisory Group-Japan.

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