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A basic flow visualization test of an F-16XL Scamp model
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A basic flow visualization test of an F-16XL Scamp model
An F-16XL Scamp model, four per cent the size of the full-scale aircraft, is tested in the Basic Aerodynamics Research Tunnel as part of a High Speed Research Program. The photograph shows a basic flow visualization test using smoke and a laser light sheet to illuminate the smoke. The tests will be used to investigate the basic flow field on the F-16XL before actual flight tests are made. The high-lift flight test program is aimed at improving performance, reducing engine noise and limiting noise exposure by using specially-designed high-lift devices on or in the wing. Even though this is a fighter-type aircraft, the sweep and general arrangement of the uniquely-designed cranked arrow wing resemble those planned for the next generation of high-speed civil transport. Flight tests of the F-16XL will allow engineers to determine the accuracy of their ground- generated information and predictive methods including wind tunnel tests, computer simulations and piloted simulations
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Aerodynamic Analysis Blue Experiment Flight Dynamics Flowing Fluid Dynamics Indoors Inspecting Laboratory Laser Model Pattern Physics Prototype Research Static Stationary Studying Test Tunnel Velocity Wind Tunnel Airflow
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This print showcases a basic flow visualization test of an F-16XL Scamp model, conducted as part of a groundbreaking High Speed Research Program. The F-16XL Scamp model, scaled down to just four percent of the full-scale aircraft, is being tested in the Basic Aerodynamics Research Tunnel. In this image, we witness the utilization of smoke and a laser light sheet to illuminate the smoke for flow visualization purposes. These tests are crucial in understanding and investigating the fundamental flow field on the F-16XL before actual flight tests take place. The primary objective of this high-lift flight test program is to enhance performance, reduce engine noise, and limit noise exposure by incorporating specially-designed high-lift devices on or within the wing structure. Interestingly enough, despite being a fighter-type aircraft, the sweep and overall arrangement of its uniquely-designed cranked arrow wing bear resemblance to those planned for future generations of high-speed civil transport. By conducting flight tests using the F-16XL model, engineers aim to validate their ground-generated information and predictive methods which include wind tunnel experiments, computer simulations, and piloted simulations. This comprehensive approach ensures accuracy in assessing aerodynamic characteristics and optimizing performance parameters. This remarkable photograph from Stocktrek Images not only captures an intricate moment in aviation research but also highlights humanity's relentless pursuit towards innovation and advancement in aerospace technology.
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