共 15 条
[1]
[Anonymous], 1999, BOUNDARY LAYER THEOR
[2]
Boundary-layer transition detection in a cryogenic wind tunnel using luminescent paint
[J].
JOURNAL OF AIRCRAFT,
1997, 34 (01)
:34-42
[3]
Campbell Bryan., 1994, 25th Plasmadynamics and Lasers Conference, page, P2483
[4]
Egami Y, 2005, P CEAS KATNET C KEY
[5]
Egami Y., 2006, P 12 INT S FLOW VIS
[6]
Engler R H, 1997, P C WIND TUNN WIND T, P431
[7]
Transition detection by temperature sensitive paint at cryogenic temperatures in the European Transonic Wind tunnel (ETW)
[J].
ICIASF'03 RECORD: 20TH INTERNATIONAL CONGRESS ON INSTRUMENTATION IN AEROSPACE SIMULATION FACILITIES,
2003,
:77-88
[8]
Fey U., 2007, SPRINGER HDB EXPT FL, P537
[9]
Fey U, 2006, 44 AIAA AER SCI M EX, P514
[10]
Germain E, 2005, 43 AIAA AER SCI M EX, P0458