With the introduction of modern airplanes utilizing laminar flow, flow visualization has become an important diagnostic tool in determining aerodynamic characteristics such as surface flow direction and boundary-layer state. A refinement of the sublimating chemical technique has been developed to define both the boundary-layer transition location and the transition mode. In response to the need for flow visualization at subsonic and transonic speeds and altitudes above 20,000 feet, the liquid crystal technique has been developed. A third flow visualization technique that has been used is infrared imaging, which offers non-intrusive testing over a wide range of test conditions. A review of these flow visualization methods and recent flight results is presented for a variety of modern aircraft and flight conditions.
Developments in flow visualization methods for flight research
International Symposium ; 1989 ; Prague, Czechoslovakia
1990-01-01
Conference paper
No indication
English
Flow visualization techniques for flight research
NTRS | 1989
|Flow Visualization Techniques for Flight Research
NTIS | 1988
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Tema Archive | 1986
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