Zobrazeno 1 - 10
of 18
pro vyhledávání: '"Gianfranco Chiocchia"'
As one of the Bologna Process countries, Russia committed herself to a number of reforms carried out within the Bologna Action Lines, amomg which are the introduction of 3 cycle system of higher education, National Qualifications Frameworks developme
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::a60e51ea130336c70d1523a3d64e704a
http://hdl.handle.net/11583/2679665
http://hdl.handle.net/11583/2679665
Autor:
Gianfranco Chiocchia, Giorgio Guglieri
The job profile of the aerospace engineers in the industry as well in aviation has undergone substantial changes during the last decades. The classical designer profile has been replaced by a much more articulated one, including a plurality of activi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::4dc054da06a711301eac00d2fb94d4ce
http://hdl.handle.net/11583/2679664
http://hdl.handle.net/11583/2679664
Publikováno v:
International Journal of Non-Linear Mechanics. 38:173-199
The present paper deals with a study of the benign and catastrophic characters of the flutter instability boundary of 2-D lifting surfaces in a supersonic flow field. The objectives of this work are: (i) to contribute to a better understanding of the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::8557464d6195227f1972715863dd3955
https://doi.org/10.1016/s0020-7462(01)00054-3
https://doi.org/10.1016/s0020-7462(01)00054-3
Publikováno v:
Aerospace Science and Technology. 6:259-272
This paper deals with the generation and use of proper aerodynamic indicial functions toward the aeroelastic formulation of two-dimensional lifting surfaces in the subsonic compressible, linearized transonic, supersonic and hypersonic flight speed re
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::478cb6c5174b3b963bba82b82625e7f4
https://doi.org/10.1016/s1270-9638(02)01169-0
https://doi.org/10.1016/s1270-9638(02)01169-0
Publikováno v:
Politecnico di Torino-IRIS
Scopus-Elsevier
Scopus-Elsevier
An unsteady linear lifting line method for the determination of the circulation and lift distribution along the span of a curved wing subject to harmonic small amplitude oscillations is presented. The method relies on the Pistolesi- Weissinger 3/4-ch
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9c9841344c992d3648ed4207cfb474e4
https://doi.org/10.1002/zamm.19970770419
https://doi.org/10.1002/zamm.19970770419
Autor:
S. Pignataro, Gianfranco Chiocchia
Publikováno v:
The Aeronautical Journal. 99:328-336
The aerodynamic interaction between a wing and a couple of propellers in tractor configuration is investigated by means of a model based on the lifting line concept and under the assumption of quasi-steady incompressible motion of inviscid fluid. The
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fc1f1c7e9a17a089e011f4504dbd0546
https://doi.org/10.1017/s0001924000028578
https://doi.org/10.1017/s0001924000028578
Publikováno v:
Politecnico di Torino-IRIS
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::7bf4c9fb561885624fef675462b03688
http://hdl.handle.net/11583/2429198
http://hdl.handle.net/11583/2429198
Publikováno v:
Politecnico di Torino-IRIS
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=dedup_wf_001::42cb35d850142113dbc5bcc1a6d83834
http://hdl.handle.net/11583/2375138
http://hdl.handle.net/11583/2375138
Publikováno v:
57th International Astronautical Congress.
The SEEDS Initiative, originated from the Politecnico di Torino with the support of Alenia Spazio, is aimed at establishing an International Master Course focussed on Space Exploration and Development Systems, to offer an opportunity for young engine
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8f65597f2169cfbb0f60a5540231952c
https://doi.org/10.2514/6.iac-06-e1.5.08
https://doi.org/10.2514/6.iac-06-e1.5.08
An aeroelastic formulation of 2D lifting surfaces in an incompressible flow field via the use of aerodynamic indicial functions is presented. The approach carried out in time and frequency domains yields the proper aerodynamic loads necessary to the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3053b080f3802f8b6e64df404dbd3a89
http://hdl.handle.net/11583/1500089
http://hdl.handle.net/11583/1500089