Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Christopher M. Heath"'
Autor:
Ben D. Phillips, Christopher M. Heath
Publikováno v:
AIAA AVIATION 2020 FORUM.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d971ea28c568fc8e87679cc22abb6816
https://doi.org/10.2514/6.2020-2730
https://doi.org/10.2514/6.2020-2730
Publikováno v:
Journal of Aircraft. 54:1283-1293
Propulsion integration for low-boom supersonic aircraft requires careful inlet selection, placement, and tailoring to achieve acceptable propulsive and aerodynamic performance, without compromising vehicle sonic boom loudness levels. In this investig
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::559cf03159eaadea329d8a92e2bd38e0
https://doi.org/10.2514/1.c034036
https://doi.org/10.2514/1.c034036
Autor:
Christopher M. Heath
Publikováno v:
Journal of Propulsion and Power. 32:500-515
Aviation gas-turbine combustion demands high efficiency, wide operability, and minimal trace gas emissions. Performance critical design parameters include injector geometry, combustor layout, fuel–air mixing, and engine cycle conditions. The presen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b9063c0c120c00a0edbadd715798c223
https://doi.org/10.2514/1.b35867
https://doi.org/10.2514/1.b35867
Publikováno v:
2018 Fluid Dynamics Conference.
Reynolds Averaged Navier-Stokes (RANS) simulations were performed on a Lockheed Martin Quiet SuperSonic Technology (QueSST) aircraft preliminary design to assess inlet performance. The FUN3D flow solver and its adjoint-based grid refinement capabilit
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d638ebdcf1116f3181d85827cad1b7e1
https://doi.org/10.2514/6.2018-3861
https://doi.org/10.2514/6.2018-3861
Publikováno v:
35th AIAA Applied Aerodynamics Conference.
Aerodynamic shape optimization is demonstrated to tailor the under-track pressure signature of a conceptual low-boom supersonic aircraft. Primarily, the optimization reduces nearfield pressure waveforms induced by propulsion integration effects. For
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::89a57e85470fad9f371460db0babe9d8
https://doi.org/10.2514/6.2017-3046
https://doi.org/10.2514/6.2017-3046
Autor:
Colin Summers, Gazi Sakib, Nariman Sharifrazi, Justin S. Gray, Robert D. Falck, Golda Nguyen, Andi Peng, Kenneth Decker, Andrew Oberlander, Christopher M. Heath, Jeffrey C. Chin
Publikováno v:
55th AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44ae51f2b7d84420ac3819771a80b60e
https://doi.org/10.2514/6.2017-0221
https://doi.org/10.2514/6.2017-0221
Autor:
Kathleen M. Tacina, Andreas J. Beyersdorf, Christopher M. Heath, D. L. Bulzan, Simon E. Albo, Luke D. Ziemba, Bruce E. Anderson, R. C. Miake-Lye, Kenneth L. Thornhill, Hsi-Wu Wong, Edward L. Winstead, R. C. Ross
Publikováno v:
Atmospheric Chemistry and Physics, Vol 13, Iss 19, Pp 10049-10060 (2013)
Contrails and contrail-induced cirrus clouds are identified as the most uncertain components in determining aviation impacts on global climate change. Parameters affecting contrail ice particle formation immediately after the engine exit plane (< 5 s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::47dd0f255b51a38e0c783ee41b78eb4b
https://doi.org/10.5194/acp-13-10049-2013
https://doi.org/10.5194/acp-13-10049-2013
Autor:
Christopher M. Heath
Publikováno v:
54th AIAA Aerospace Sciences Meeting.
Aviation gas-turbine combustion demands high efficiency, wide operability and minimal trace gas emissions. Performance critical design parameters include injector geometry, combustor layout, fuel-air mixing and engine cycle conditions. The present in
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::fabf4ebc8a22db165dc30c41842726ac
https://doi.org/10.2514/6.2016-1394
https://doi.org/10.2514/6.2016-1394
Publikováno v:
53rd AIAA Aerospace Sciences Meeting.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d311e072f72a7411b93daa7aa8003cf1
https://doi.org/10.2514/6.2015-1047
https://doi.org/10.2514/6.2015-1047
Publikováno v:
52nd Aerospace Sciences Meeting.
Fundamental research for sonic boom reduction is needed to quantify the interaction of shock waves generated from the aircraft wing or tail surfaces with the nozzle exhaust plume. Aft body shock waves that interact with the exhaust plume contribute t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::c637dd9c2e5ad79f0f194dbce6cb2f37
https://doi.org/10.2514/6.2014-0232
https://doi.org/10.2514/6.2014-0232