Zobrazeno 1 - 10
of 26
pro vyhledávání: '"W. H. Wentz"'
Autor:
W. H. Wentz, Ahmed S. Mohamed
Publikováno v:
SAE Technical Paper Series.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::90396bffaad9554c984bcbce73234c19
https://doi.org/10.4271/2008-01-2225
https://doi.org/10.4271/2008-01-2225
Publikováno v:
AIAA 5th ATIO and16th Lighter-Than-Air Sys Tech. and Balloon Systems Conferences.
Hydrogen is receiving increasing attention as a potential transportation fuel, as a result of environmental and supply issues with conventional hydrocarbon fuels. Coupling fuel cells with electric motors provides an energy system for propulsion that
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2a2526a82b08f4571136ecf1bf26af6a
https://doi.org/10.2514/6.2005-7324
https://doi.org/10.2514/6.2005-7324
Autor:
Ahmed S. Mohamed, W. H. Wentz
Publikováno v:
SAE Technical Paper Series.
Global warming concerns are stimulating accelerated research and development of alternative fuels and propulsion systems for automobiles. The potential application of these emerging technologies to airplanes is reviewed. Preliminary designs of zero g
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5f1447fefd07e4d89d12099b71456deb
https://doi.org/10.4271/2004-01-1803
https://doi.org/10.4271/2004-01-1803
Publikováno v:
Flight Simulation Technologies Conference and Exhibit.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::690dead12eaf54c6c1f9a873fa421c24
https://doi.org/10.2514/6.1990-3021
https://doi.org/10.2514/6.1990-3021
Autor:
W. H. Wentz, H. C. Seetharam
Publikováno v:
Journal of Aircraft. 14:51-55
Detailed measurements of flow fields associated with low-speed turbulent boundary layers have been made for the 17% thick GA(W)-1 airfoil section at nominal angles of attack of 10, 14, and 18 deg; Reynolds number 2.2 million; and Mach number 0.13. Th
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::23ec3e4eb233eea8e824990fdbc8ba45
https://doi.org/10.2514/3.44573
https://doi.org/10.2514/3.44573
Autor:
W. H. Wentz, David Manor
Publikováno v:
Journal of Aircraft. 22:78-82
The effects of sideslip on the performance and stability of a double-delta wing and wing-body configuration were determined experimentally. The wake total pressure reveals the vortex size, location, and shape. Sideslip angle resulted in a decreased s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ec6447195f8b67d50c8dea54dd519517
https://doi.org/10.2514/3.45083
https://doi.org/10.2514/3.45083
Publikováno v:
Journal of Aircraft. 26:979-985
Flight tests were conducted at three different altitudes to detect transition on a smoothed test region of a swept-wing business jet wing using surface hot-film sensors and sublimating chemicals. Strong influence of sweep angle on transition location
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::787fedcc8e3065e656d90245696327ab
https://doi.org/10.2514/3.45870
https://doi.org/10.2514/3.45870
Autor:
W. H. Wentz, D. L. Kohlman
Publikováno v:
Journal of Aircraft. 8:156-161
Vortex breakdown on slender sharp edged and modified delta wings with varying sweep angles investigated in wind tunnel using schlieren system for flow visualization
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::44066a87f959b4c936615a67dfb2a347
https://doi.org/10.2514/3.44247
https://doi.org/10.2514/3.44247
Autor:
W. G. Thomson, W. H. Wentz
Publikováno v:
SAE Technical Paper Series.
The results of an analytical study of aerodynamic interference effects for a light twin aircraft are presented. The data presented concentrates on the influence of a wing on a body (the fuselage). Wind tunnel comparisons of three fillets are included
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::924cd9f413357132b798597caf3709c9
https://doi.org/10.4271/830709
https://doi.org/10.4271/830709
Publikováno v:
2nd Applied Aerodynamics Conference.
Flight test experiments have been conducted to measure the extent and nature of laminar flow on a smoothed test region of a swept-wing business jet. Surface hot film anemometers and sublimating chemicals were used for transition detection. Surface pr
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f194411697330b785144b97d5a3c62f5
https://doi.org/10.2514/6.1984-2189
https://doi.org/10.2514/6.1984-2189