Zobrazeno 1 - 10
of 81
pro vyhledávání: '"Mach tuck"'
Publikováno v:
Aerospace, Vol 9, Iss 8, p 411 (2022)
The recent improvement of technology readiness level in aeronautics and the renewed demand for faster transportation are driving the rebirth of supersonic flight for commercial aviation. However, the design of a future supersonic aircraft is still ve
Externí odkaz:
https://doaj.org/article/23ea95d162464b5bb7d0501fa971e44c
Akademický článek
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Autor:
Martin Rein, Michael Paul
Publikováno v:
Journal of Aircraft. 54:1139-1149
Lambda wing configurations are known to possess challenging flight characteristics at transonic Mach numbers. This study tests various methods for increasing the maneuverability and stability of the SACCON, a generic lambda wing configuration. Severa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::43bc93fcc35cfd976e40cc7e95b38a51
https://doi.org/10.2514/1.c034080
https://doi.org/10.2514/1.c034080
Autor:
L. V. Morozov
Publikováno v:
Russian Aeronautics (Iz VUZ). 58:100-105
This paper considers the equilibrium condition of a winged aircraft cable-towed by a carrier in level flight at a subsonic speed. A technique is suggested to determine the geometric parameters of a tapered wing according to vehicle mass within the su
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::11fb95695f549cef85dca0862dd805a3
https://doi.org/10.3103/s106879981501016x
https://doi.org/10.3103/s106879981501016x
Publikováno v:
47th AIAA Fluid Dynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::57e2db21b0d7dcddb1359484f043553f
https://doi.org/10.2514/6.2017-3967
https://doi.org/10.2514/6.2017-3967
Autor:
Yi Jiang, Rui Qing Liu
Publikováno v:
Advanced Materials Research. :1331-1336
Rocket engine thrust is the main performance parameters. The flow field of missile fight in different Mach is simulated by using FLUENT, then calculating the thrust of different conditions. The calculating results are consistent with the theory of Ma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d9224571c846151573baf6816b7dd15b
https://doi.org/10.4028/www.scientific.net/amr.1030-1032.1331
https://doi.org/10.4028/www.scientific.net/amr.1030-1032.1331
Publikováno v:
CEAS Aeronautical Journal. 5:305-317
Over-the-wing propeller configurations and particularly channel wing concepts show increased climb performance, and through effective acoustic shielding, reduced noise emissions when compared to a conventional tractor configuration. The main aerodyna
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::341e7ff3db5ed64dcb92c520001c4d73
https://doi.org/10.1007/s13272-014-0108-1
https://doi.org/10.1007/s13272-014-0108-1
Autor:
Yue Min Yu
Publikováno v:
Advanced Materials Research. :1764-1767
This paper discusses the design of a section morphing wing that permits a change in the wing section while simultaneously supporting structural wing loads. Section morphing wing allows for two discreet airfoil of the wing. The airfoil 1 is original a
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4a0fbf73e2839f33bd44a990f272b087
https://doi.org/10.4028/www.scientific.net/amr.753-755.1764
https://doi.org/10.4028/www.scientific.net/amr.753-755.1764
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2e33b653bbfb093c92e7d527a75dac58
https://doi.org/10.2514/6.2017-0266
https://doi.org/10.2514/6.2017-0266
Publikováno v:
Journal of Aerospace Engineering. 25:600-612
The potential positive influence of close ground proximity on the aerodynamic performance of a wing has long been established; however, flight at a Mach number that causes shock waves to form between the wing and the ground plane would have significa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1d776064db8897bf090354aced3a8740
https://doi.org/10.1061/(asce)as.1943-5525.0000169
https://doi.org/10.1061/(asce)as.1943-5525.0000169