Zobrazeno 1 - 10
of 217
pro vyhledávání: '"John D. Berry"'
Autor:
BERRY, JOHN D.
Publikováno v:
U & lc; Summer98, Vol. 25 Issue 1, p38-42, 2p, 3 Color Photographs
Publikováno v:
Journal of Aircraft. 39:645-653
Development of advanced rotorcraft configurations has highlighted a need for high-quality experimental data to support the development of robust and accurate analytical design tools. To provide high-quality experimental data, a test program was condu
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2bb96dae424479771fdee2119a2e21d6
https://doi.org/10.2514/2.2977
https://doi.org/10.2514/2.2977
Autor:
John D. Berry, Mark S. Chaffin
Publikováno v:
Journal of the American Helicopter Society. 42:235-243
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e9468bda8497c4cdd960fe6b0394c57
https://doi.org/10.4050/jahs.42.235
https://doi.org/10.4050/jahs.42.235
Autor:
John D. Berry
Publikováno v:
International Journal of Multicultural Education. 13
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8a2587524097a8e56e19c32fc029fe05
https://doi.org/10.18251/ijme.v13i2.471
https://doi.org/10.18251/ijme.v13i2.471
Automated systems to perform aircraft diagnostics and prognostics are of current interest. Development of those systems requires large amounts of data (collection, monitoring, manipulation) to capture and characterize fault events, and to ensure data
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::39528e6262a72cca19e0ae43d42a9550
https://doi.org/10.21236/ada501579
https://doi.org/10.21236/ada501579
Autor:
Michael A. McVeigh, Jacob Wilson, Redstone Arsenal, John D. Berry, Aeroflightdynamics Directorate, Marty Moulton, Tin-Chee Wong, Preston B. Martin
Publikováno v:
26th AIAA Applied Aerodynamics Conference.
The passive control of compressible dynamic stall has been experimentally demonstrated in a dynamically oscillating airfoil test at Reynolds numbers near two million and Mach numbers ranging from M = 0.3 to 0.4. A rotorcraft-type airfoil was retrofit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::11a971d1a6fa796d11ea0b3c4f9e46cc
https://doi.org/10.2514/6.2008-7506
https://doi.org/10.2514/6.2008-7506
Publikováno v:
2005 IEEE Aerospace Conference.
The US Army relies heavily on their helicopter fleet to provide close air support, troop transport, reconnaissance and logistics support capabilities for a variety of mission profiles. High operational readiness and availability of the helicopter fle
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a5907a4d95ab5a8ed8cb880579722488
https://doi.org/10.1109/aero.2005.1559681
https://doi.org/10.1109/aero.2005.1559681
Publikováno v:
2003 IEEE Aerospace Conference Proceedings (Cat. No.03TH8652).
Automated systems to perform aircraft diagnostics and prognostics are of current interest. Development of those systems requires large amounts of data (collection, monitoring, manipulation) to capture and characterize normal, known fault events, and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::147b788100911c08ecb73a5726bd90d0
https://doi.org/10.1109/aero.2003.1234178
https://doi.org/10.1109/aero.2003.1234178
Publikováno v:
Proceedings, IEEE Aerospace Conference.
A key to producing reliable engine diagnostics and prognostics resides in fusion of multisensor data. It is believed that faults will manifest effects in a variety of sensors. By 'integration' (fusion) of information across sensors detections can be
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::27bd27dc3c52ca09a0a1b4c5a4a8ffd0
https://doi.org/10.1109/aero.2002.1036145
https://doi.org/10.1109/aero.2002.1036145
Publikováno v:
2000 IEEE Aerospace Conference. Proceedings (Cat. No.00TH8484).
Helicopter rotor smoothing (track and balance) is a periodic maintenance task required to minimize rotor induced aircraft vibrations at the fundamental (once per revolution) rotor frequency. We have designed and implemented a general, neural network
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dc7ab7bc9941953c444098c27a8e0732
https://doi.org/10.1109/aero.2000.877903
https://doi.org/10.1109/aero.2000.877903