Zobrazeno 1 - 8
of 8
pro vyhledávání: '"U. W. Schaub"'
Publikováno v:
Journal of Turbomachinery. 112:286-293
The present work was conducted to extend information derived in a previous study where it was found that the performance of a transonic turbine nozzle of high turning angle was significantly affected by the design and operation of the downstream roto
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::aa7263c8cebd83b83953da5cd5cd7dc9
https://doi.org/10.1115/1.2927651
https://doi.org/10.1115/1.2927651
Publikováno v:
Journal of Applied Mechanics. 30:518-524
The application of moderate pressure gradients can exercise a large influence on the decay of wakes produced by obstructions in a flow field. In fact, a positive pressure gradient may arrest completely the decay process and cause the relative wake si
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1c06129eef4b70f52250e8d5f847fa25
https://doi.org/10.1115/1.3636612
https://doi.org/10.1115/1.3636612
Ram Air Effects on the Air Side Cooling System Performance of a Typical North American Passenger Car
Autor:
U. W. Schaub, H. N. Charles
Publikováno v:
SAE Technical Paper Series.
A standard engine mounted cooling fan in a 1976 Ford Granada equipped with air conditioning and a 4.91 (302 cu. in.) V-8 engine was performance-tested on the road and under wind tunnel generated ram air conditions. To achieve appropriate back pressur
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d272b075117d6e4aebda81b06e2953d1
https://doi.org/10.4271/800032
https://doi.org/10.4271/800032
Autor:
U. W. Schaub, G. Krishnappa
Publikováno v:
4th Aeroacoustics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::819e6d53d9f300521b9a3d466348ee13
https://doi.org/10.2514/6.1977-1362
https://doi.org/10.2514/6.1977-1362
Autor:
U. W. Schaub, A. N. Abdelhamid
Publikováno v:
ASME 1972 International Gas Turbine and Fluids Engineering Conference and Products Show.
Unsteady forces and noise from a fan-in-wing model operated in cross flow are investigated. Based on experimentally determined inlet and outlet flow distortions the unsteady forces on the rotor blades are determined analytically taking into account t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7edb506ea1895c665971cf1bba8770fa
https://doi.org/10.1115/72-gt-92
https://doi.org/10.1115/72-gt-92
Autor:
U. W. Schaub
Publikováno v:
10th Anglo-American Aeronautical Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::86ca0f0b672b65d23c2b24eedad3f3ce
https://doi.org/10.2514/6.1967-746
https://doi.org/10.2514/6.1967-746
Autor:
U. W. Schaub
Publikováno v:
Journal of Engineering for Power. 97:9-9
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b5f83503451c628d12b77b18310349cd
https://doi.org/10.1115/1.3445930
https://doi.org/10.1115/1.3445930
Autor:
U. W. Schaub
Publikováno v:
Journal of Engineering for Power. 96:322-322
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a61ae475281e9f1bda962404c0940861
https://doi.org/10.1115/1.3445841
https://doi.org/10.1115/1.3445841