Zobrazeno 1 - 10
of 14
pro vyhledávání: '"Masashi SHIGEMI"'
Publikováno v:
Journal of Aircraft. 57:889-900
This Paper describes a new method of correcting the wind tunnel wall interference of permeable Kevlar test section walls. The classical three-dimensional panel method is extended to flows in a Kevl...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::df64a256162d1fcaad02ce0a7ef79f14
https://doi.org/10.2514/1.c035864
https://doi.org/10.2514/1.c035864
Publikováno v:
25th AIAA/CEAS Aeroacoustics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::411fdc4eb487ee6d8eb4954b3f94640c
https://doi.org/10.2514/6.2019-2698
https://doi.org/10.2514/6.2019-2698
Publikováno v:
Journal of Aircraft. Sep2020, Vol. 57 Issue 5, p889-900. 12p.
Publikováno v:
JOURNAL OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES. 53:325-329
The Pitot probe with 5-hole pyramidal head originally developed by NAL was planed to be adopted in the early phase of the development of the High-Speed Flight Demonstration Phase II. But it was turned out that the probe could not achieve enough abili
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::72e2d9980b29d4d5ee7e524bc1387c55
https://doi.org/10.2322/jjsass.53.325
https://doi.org/10.2322/jjsass.53.325
Publikováno v:
Journal of Aircraft. 40:164-172
Effects of test section sidewalls have been investigated in a two-dimensional transonic wind tunnel. The facility has recently been modie ed to improvethe e ow two dimensionality for airfoil testing. A procedure where two Mach number corrections for
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d8e1b1c0e2137b1b1375b3c109077839
https://doi.org/10.2514/2.3071
https://doi.org/10.2514/2.3071
Publikováno v:
Journal of Aircraft. 36:926-933
The Automatic Landing Flight Experiment (ALFLEX) project was conducted as part of the research on the H-II orbiting plane-experimental (HOPE-X) unmanned reentry vehicle. One of the aims of the ALFLEX was to estimate the low-speed aerodynamic characte
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bdabff65031370259f87b0946da19d9c
https://doi.org/10.2514/2.2553
https://doi.org/10.2514/2.2553
Publikováno v:
Journal of the Japan Society for Aeronautical and Space Sciences. 46:29-36
One of the purposes of the Automatic Landing Flight Experiment (ALFLEX) was to estimate low-speed aerodynamic characteristics of a vehicle with a delta wing and tip fins. The tests for this purpose, such as a I /? sweep tests and control surface exci
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c94ae177602894ff37406ac0df33a748
https://doi.org/10.2322/jjsass1969.46.29
https://doi.org/10.2322/jjsass1969.46.29
Autor:
Yukimitsu Yamamoto, Yasutoshi Inouye, Shigeya Watanabe, Masashi Shigemi, Masao Shirouzu, Makoto Ueno, Takeshi Ito
Publikováno v:
34th AIAA Fluid Dynamics Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d7ed2c9ff4a605d21e6a609da1b5c166
https://doi.org/10.2514/6.2004-2426
https://doi.org/10.2514/6.2004-2426
Publikováno v:
19th AIAA Applied Aerodynamics Conference.
Effects of test section sidewalls have been investigated in a two-dimensional transonic wind tunnel. The facility has recently been modified to improve the flow two-dimensionality for airfoil testing. A procedure where two corrections for top and bot
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b680f38d109b39a8562c8d8a0f5a3060
https://doi.org/10.2514/6.2001-2423
https://doi.org/10.2514/6.2001-2423
Publikováno v:
22nd Atmospheric Flight Mechanics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::36bdece55bb458680c7dbc043066d6c7
https://doi.org/10.2514/6.1997-3485
https://doi.org/10.2514/6.1997-3485