Zobrazeno 1 - 3
of 3
pro vyhledávání: '"R. W. Hensel"'
Autor:
J. S. McDaniel, M. Aguado, L. Aleman, R. H. Ammon, J. G. Anderson, A. Andreotti, G. Ardrey, P. Barker, K. Bell, E. M. Berckmiller, S. Brewer, J. Burke, G. Chapman, W. Chisholm, P. Chowdhuri, E. Cinieri, M. G. Comber, M. T. Correia De Barros, K. Cummins, F. C. De la Rosa, C. Donati, R. Clay Doyle, E. Dziedzic, G. Engmann, D. L. Flaten, M. M. Gonzalez, M. Grogan, S. Grzybowski, S. Harper, R. Hedding, R. W. Hensel, C. Hickman, M. Ishii, K. C. Jaffa, W. Janischewskyj, J. Kappenman, G. G. Karaday, M. Khodaie, J. L. Koepfinger, D. Moreira Leite, V. Longo, D. Maltempi, J. A. Martinez Velasco, M. Marz, K. Matsuda, T. McDermott, R. E. Moore, R. Newman, D. Nichols, D. J. Pearson, L. Perez, G. Podporkin, F. Rachidi, V. A. Rakov, E. R. Ross J.r., T. J. Rozek, J. M. Santuk, T. Schehade, T. A. Short, K. Shortt, M. H. Shwehdi, L. S. Taylor, C. Tirado, R. A. Walling, D. J. Ward, C. A. Warren, L. Welch, C. W. Williams, J. J. Woodworth, W. N. Zessin, BORGHETTI, ALBERTO, NUCCI, CARLO ALBERTO, PAOLONE, MARIO
Measures for improving the lightning protection performance of schemes applied to overhead power distribution lines are discussed in this guide.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______4094::6cf4ecf00060b09413f3b7bff0db3264
http://hdl.handle.net/11585/20119
http://hdl.handle.net/11585/20119
Autor:
J. G. GAVIN, R. W. HENSEL
Publikováno v:
Journal of the Aeronautical Sciences. 9:533-537
The tunnel-wall effects on drag and stall, given by the usual simple corrections, are not adequate when the span-diameter ratio is high or when the spanwise lift distribution varies considerably from elliptical. In order to determine more exact inter
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd7c11af40f8e2b0219e7ba3216d35fc
https://doi.org/10.2514/8.10961
https://doi.org/10.2514/8.10961
Autor:
M. Pindzola, R. W. Hensel
Publikováno v:
The Aeronautical Journal. 74:197-205
The purpose of this paper is to further illustrate the utility of a wind tunnel (see refs. 1 and 2) in providing performance date on aircraft engine installations. The discussion is limited to the test work accomplished in the Propulsion, Wind Tunnel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9e6592ea38cb2b9133fd353289d54e5d
https://doi.org/10.1017/s0001924000113946
https://doi.org/10.1017/s0001924000113946