Zobrazeno 1 - 6
of 6
pro vyhledávání: '"Antonio De La Garza"'
Autor:
Miguel A. Medina-Morales, Sócrates Palacios Ponce, José Antonio De La Garza-Rodríguez, Leopoldo J. Ríos-González, Marisol Cruz-Requena
Publikováno v:
Practical Applications of Physical Chemistry in Food Science and Technology
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a61cf6782bb8b579a8e8e6a72d8db7a4
https://doi.org/10.1201/9781003020004-10
https://doi.org/10.1201/9781003020004-10
Autor:
Walter A. Silva, Mark D. Sanetrik, Michael Buonanno, Pawel Chwalowski, Paul Scott Zink, Seung Yeun Yoo, David M. Christhilf, Antonio De La Garza, James R. Florance, J. C. Johnson, George Kopasakis, Jiyoung Hur, Elias G. Bounajem
Publikováno v:
56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
An overview of NASA’s High Speed Aeroservoelasticity (ASE) project is provided with a focus on recent computational aeroelastic analyses of a low-boom supersonic configuration developed by Lockheed-Martin and referred to as the N+2 configuration. T
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::6cd543240b59406f3fbe73c6519bfb5f
https://doi.org/10.2514/6.2015-0684
https://doi.org/10.2514/6.2015-0684
Publikováno v:
12th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference and 14th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference.
As design requirements and affordability for future aircraft become increasingly demanding, aircraft design processes will be required to explore a larger design space and capture multi-disciplinary effects during conceptual design to effectively ass
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e1c588f235217fc18090fd64ff2b582d
https://doi.org/10.2514/6.2012-5490
https://doi.org/10.2514/6.2012-5490
Autor:
Antonio De La Garza, Slater Voorhees, Christopher Reed, Michael Skillen, Wright-Patterson Afb, Richard D. Snyder, Scott Zink
Publikováno v:
51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th.
Through funding from the Air Force Research Laboratory, a wing tip-tail configuration for a future re-usable launch vehicle demonstrator was designed, structurally-sized through finite element based approaches, and then analyzed for aeroelastic perfo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7813aaf824e0fda8f19d747c6b99addb
https://doi.org/10.2514/6.2010-2953
https://doi.org/10.2514/6.2010-2953
Publikováno v:
50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The flexible body dynamics of wing bending (both vertical and fore -aft modes) for high aspect ratio blended wing -body tailless aircraft challenges the traditional nonlinear flight con trol system design process. The frequencies associated with thes
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d6c7b564e5831b6add572f067a395777
https://doi.org/10.2514/6.2009-2405
https://doi.org/10.2514/6.2009-2405
Publikováno v:
26th AIAA Applied Aerodynamics Conference.
The flexible body dynamics of wing bending (both vertical and fore -aft modes) for high aspect ratio blended wing -body tailless aircraft challenge s the traditional nonlinear flight cont rol system design process. The frequencies associated with the
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f8a923215d570b308a8d4ed32e7b5d3c
https://doi.org/10.2514/6.2008-7188
https://doi.org/10.2514/6.2008-7188