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| F-111A in flight | ||
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| Photo Number: | ECN-2092 | |
| Photo Date: | July 10, 1968 | |
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| Formats: | 558x480 JPEG Image (57 KBytes) 1191x1024 JPEG Image (473 KBytes) 2000x1720 JPEG Image (549 KBytes) |
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| Description: |
This late 1960s photograph shows an early General Dynamics F-111A Aardvark in flight at the NASA Flight Research Center. The wings on this aircraft did not have a supercritical airfoil design. In 1967 the NASA Flight Research Center received the first of two F-111A aircraft (the number six prototype, Serial #63-9771) to evaluate. These early F-111s had problems with their engines and suffered from repeated compressor surges and stalls. After extensive testing, NASA, the Air Force, and General Dynamics arrived at a major inlet redesign to resolve the problems. The second F-111A (#63-9777) arrived at the Center in 1969 and was used for a handling-qualities study. |
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| Keywords: | F-111A; F-111E; Aardvark; General Dynamics F-111A Aardvark; NASA Dryden Flight Research Center; Air Force; Transonic Aircraft Technology; TACT; Mission Adaptive Wing; MAW; Dr. Richard Whitcomb; Supercritical Wing; NASA Langley Research Center;Integrated Propulsion Control System; IPCS; Advanced Fighter TechnologyIntegration; AFTI; Digital Electronic Engine Control; DEEC; Air Force Flight Dynamics Laboratory; Air Force Flight Propulsion Laboratory; Pratt & Whitney Company; Natural Laminar Flow. | |
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Last Modified: February 6, 2002 |
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