Pressure field testing investigation of airplane model by luminescence pressure sensor technique in high speed wind tunnel

ZHANG Yon-gcun; CHENG Hou-mei; ZHANG Ran; XING Han-qi; LI Chen

doi:10.3969/j.issn.1672-9897.2000.02.003

ZHANG Yon-gcun, CHENG Hou-mei, ZHANG Ran, XING Han-qi, LI Chen. Pressure field testing investigation of airplane model by luminescence pressure sensor technique in high speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2000, 14(2): 21-25. DOI: 10.3969/j.issn.1672-9897.2000.02.003

Citation:

ZHANG Yon-gcun, CHENG Hou-mei, ZHANG Ran, XING Han-qi, LI Chen. Pressure field testing investigation of airplane model by luminescence pressure sensor technique in high speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2000, 14(2): 21-25. DOI: 10.3969/j.issn.1672-9897.2000.02.003

Citation:

ZHANG Yon-gcun, CHENG Hou-mei, ZHANG Ran, XING Han-qi, LI Chen. Pressure field testing investigation of airplane model by luminescence pressure sensor technique in high speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2000, 14(2): 21-25. DOI: 10.3969/j.issn.1672-9897.2000.02.003

Pressure field testing investigation of airplane model by luminescence pressure sensor technique in high speed wind tunnel

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Pressure field testing investigation of airplane model by luminescence pressure sensor technique in high speed wind tunnel

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