Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Eric Y. Reichenbach"'
Autor:
Krishna Hoffman, Sally A. Viken, Neal A. Harrison, Eric D. Dickey, Michael D. Beyar, Gregory M. Gatlin, Eric Y. Reichenbach
Publikováno v:
AIAA Scitech 2020 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::710c90df431b17e7c38bd2bec93a4db5
https://doi.org/10.2514/6.2020-0011
https://doi.org/10.2514/6.2020-0011
Publikováno v:
Journal of Aircraft. 51:1580-1591
This paper reviews the applicability of some conventional structural design practices to the analysis and design of very flexible aircraft. The effect of large structural deformations and the coupling between aeroelasticity and flight dynamics is inv
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cee81d66bdd60c4be22d667ce6bb3976
https://doi.org/10.2514/1.c032464
https://doi.org/10.2514/1.c032464
Publikováno v:
AIAA Infotech@Aerospace 2010.
The Dynamic Flight Envelope Assessment and Prediction (DFEAP) program is a NASA funded research effort being conducted as part of NASA’s Aviation Safety Program. The goal of the DFEAP program is to provide a computational framework which will provi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ca779da29597de1d365d39b4aeda9cff
https://doi.org/10.2514/6.2010-3343
https://doi.org/10.2514/6.2010-3343
Publikováno v:
AIAA Guidance, Navigation and Control Conference and Exhibit.
1. Summary This paper will discuss a three year research program being conducted by the Boeing Phantom Works, St. Louis, MO. This program addresses the NASA Integrated Resilient Aircraft Control (IRAC) Topic 1.3, Dynamic Flight Envelope Assessment an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::12e0ca37c54486c4ce43be5d72a92430
https://doi.org/10.2514/6.2008-6983
https://doi.org/10.2514/6.2008-6983
Publikováno v:
43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference.
The left wing of the Active Aeroelastic Wing (AAW) F/A-18 airplane has been ground-load-tested to quantify its torsional stiffness. The test has been performed at the NASA Dryden Flight Research Center in November 1996, and again in April 2001 after
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::47470989aabcb8fc4ae7e2c0bd54c23b
https://doi.org/10.2514/6.2002-1333
https://doi.org/10.2514/6.2002-1333