Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Stephen G. Shaw"'
Publikováno v:
32nd AIAA Applied Aerodynamics Conference.
Phase II of a two-phase study is described that designs and validates a supersonic airliner feasible for entry into service in the 2018 to 2020 timeframe (NASA N+2 generation). A Mach 1.6 to 1.8 low sonic-boom aircraft configuration is further develo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::939a50fddf5322d8678536b92083bf32
https://doi.org/10.2514/6.2014-2137
https://doi.org/10.2514/6.2014-2137
Publikováno v:
AIAA Ground Testing Conference.
In an effort to identify test facilities that offer sonic boom measurement capabilities, an exploratory test program was initiated using wind tunnels at NASA research centers. The subject of this report is the sonic boom pressure rail data collected
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::786844cd464c66f7cd13db6a991ff326
https://doi.org/10.2514/6.2013-3122
https://doi.org/10.2514/6.2013-3122
Publikováno v:
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition.
A two-phase study is described that designs and validates a supersonic airliner feasible for entry into service in the 2018 to 2020 timeframe (NASA N+2 generation). A Mach 1.6 to 1.8 low sonic-boom aircraft configuration is developed that meets aggre
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::104bf6816c56b07e0e1122caccb207b8
https://doi.org/10.2514/6.2013-646
https://doi.org/10.2514/6.2013-646
Publikováno v:
Southern Medical Journal. 94:1215-1216
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::264893f41d555685d0104ec99d3134ac
https://doi.org/10.1097/00007611-200194120-00018
https://doi.org/10.1097/00007611-200194120-00018