Zobrazeno 1 - 10
of 10
pro vyhledávání: '"NV Taylor"'
Publikováno v:
Acta Astronautica. 66:550-562
This paper provides an overview of results generated by the static test expansion–deflection rocket nozzle (STERN) project. The engine propellants were gaseous air and hydrogen, with a design chamber pressure and thrust of 102 bar and 5 kN respecti
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ed2e841ce2fe3bfb255724303e5b9092
https://doi.org/10.1016/j.actaastro.2009.07.016
https://doi.org/10.1016/j.actaastro.2009.07.016
Autor:
Christian B Allen, M. J. de C. Henshaw, I. Kaynes, NV Taylor, Abdul Rampurawala, Ann L Gaitonde, Jonathan E. Cooper, D. S. Amor, Mark Woodgate, Grigorios Dimitriadis, Dorian P Jones, CL Fenwick, Ken Badcock, C. J. Denley, Gareth A. Vio, T. A. Eccles, J. Chamberlain
Publikováno v:
Progress in Aerospace Sciences. 43:65-137
Current industrial practice for the prediction and analysis of flutter relies heavily on linear methods and this has led to overly conservative design and envelope restrictions for aircraft. Although the methods have served the industry well, it is c
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9ac16a23fbd6af3f80239755f89afa6e
https://doi.org/10.1016/j.paerosci.2007.05.002
https://doi.org/10.1016/j.paerosci.2007.05.002
Autor:
Mark Woodgate, Jonathan E. Cooper, M. J. de C. Henshaw, NV Taylor, Abdul Rampurawala, Dorian P Jones, Christian B Allen, Ann L Gaitonde, Gareth A. Vio, Ken Badcock
Publikováno v:
The Aeronautical Journal. 110:333-343
This paper presents a comparison of linear and non-linear methods for the analysis of aeroelastic behaviour and flutter boundary prediction. The methods in question include NASTRAN and ZAERO, based on linear aerodynamics, and the non-linear coupled C
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a934ff82e19760063ea4b41de3f28391
https://doi.org/10.1017/s0001924000013208
https://doi.org/10.1017/s0001924000013208
Publikováno v:
International Journal for Numerical Methods in Engineering. 64:1628-1648
The prediction of the flutter boundary of an aircraft is a necessary but time consuming process, particularly as for the most realistic results a time accurate simulation of the interaction between the non-linear aerodynamic and structural forces is
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::32ba476a2b313be3710b634d141edd8e
https://doi.org/10.1002/nme.1421
https://doi.org/10.1002/nme.1421
Autor:
CM Hempsell, NV Taylor
Publikováno v:
The Aeronautical Journal. 108:515-522
While expansion deflection (ED) nozzles have traditionally been considered primarily for use as altitude compensating devices to improve the performance of single stage to orbit vehicles, they also offer the potential for enhancing high altitude prop
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::78ea69f427df1943b89b24006de8f586
https://doi.org/10.1017/s0001924000000348
https://doi.org/10.1017/s0001924000000348
Publikováno v:
The Aeronautical Journal. 108:389-401
Aeroelastic analysis is a critical area of the aircraft design process, as a good understanding of the dynamic behaviour of the wing structure is essential to safe operation of the vehicle. The inevitable inaccuracies present in the modelling of such
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::eccf16e8ae813eba82eb2ef7ebe8659c
https://doi.org/10.1017/s0001924000000208
https://doi.org/10.1017/s0001924000000208
Autor:
CL Fenwick, Ann L Gaitonde, Dorian P Jones, V. Lee, Christian B Allen, NV Taylor, G. F J Hill
Publikováno v:
23rd AIAA Applied Aerodynamics Conference.
Initial results produced by aeroservoelastic simulations of the BACT (Benchmark Active Control Technology) wing are presented. This is a low aspect ratio wing with large trailing edge ap. A fully time-synchronised aeroelastic simulation tool has prev
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::feba4e2e536f2999b7a524904ffea1c0
https://doi.org/10.2514/6.2005-4840
https://doi.org/10.2514/6.2005-4840
Publikováno v:
22nd Applied Aerodynamics Conference and Exhibit.
Flutter clearance and aeroelastic analysis of aircraft is of vital importance, as avoidance of the non-linear phenomena involved is critical to the safe operation of an aircraft. However, the complexity of the behaviour involved makes detailed analys
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5e66319d0ee6180dd859334d8713ea3
https://doi.org/10.2514/6.2004-5370
https://doi.org/10.2514/6.2004-5370
Autor:
Jd Hardwick, Wj Sivewright, Re West, Bgr Holloway, Jed Saner, Hj Wadsworth, Jw Hunter, NV Taylor, Msa Wilson, R Daine, Mj Feit
Publikováno v:
Proceedings of the Institution of Civil Engineers. 56:63-74
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a604285580bce90efea1a72a428410a9
https://doi.org/10.1680/iicep.1974.4125
https://doi.org/10.1680/iicep.1974.4125
Autor:
NV Taylor, Pg Clutterbuck, Pg Hughes, Wj Sivewright, Ajs Mansfield, M Agar, D.E.J. Jones, De Glyn Woods, Jt Williams, Bgr Holloway, Jeg Palmer, Dj Doughty, F Irwin Childs, Pt Shaw, Jh Simpson
Publikováno v:
Proceedings of the Institution of Civil Engineers. 64:605-617
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1047628dedd41b9932cb3e6a47dc7e29
https://doi.org/10.1680/iicep.1978.2696
https://doi.org/10.1680/iicep.1978.2696