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  • Aerodynamics  (2)
  • 1995-1999  (2)
  • 1
    Publication Date: 2011-08-23
    Description: A schlieren imaging system that uses the sun as a light source was developed it) obtain direct flow-field images of shock waves of aircraft in flight. This system was used to study how shock waves evolve to form sonic booms. The image quality obtained was limited by several optical and mechanical factors. Converting the photographs to digital images and applying digital image-processing techniques greatly improved the final quality of the images and more clearly showed the shock structures.
    Keywords: Aerodynamics
    Type: Journal of Flow Visualization and Image Processing; Volume 4; 189-199
    Format: text
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  • 2
    Publication Date: 2019-07-13
    Description: Wing compression shock shadowgraphs were observed on two flights during banked turns of an L-1011 aircraft at a Mach number of 0.85 and an altitude of 35,000 ft (10,700 m). Photos and video recording of the shadowgraphs were taken during the flights to document the shadowgraphs. Bright sunlight on the aircraft was required. The time of day, aircraft position, speed and attitudes were recorded to determine the sun azimuth and elevation relative to the wing quarter chord-line when the shadowgraphs were visible. Sun elevation and azimuth angles were documented for which the wing compression shock shadowgraphs were visible. The shadowgraph was observed for high to low elevation angles relative to the wing, but for best results high sun angles relative to the wing are desired. The procedures and equations to determine the sun azimuth and elevation angle with respect to the quarter chord-line is included in the Appendix.
    Keywords: Aerodynamics
    Type: NASA/TM-1998-206551 , H-2251 , NAS 1.15:206551 , Flow Visualization; Sep 01, 1998 - Sep 04, 1998; Sorrento; Italy
    Format: application/pdf
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