Cite
Pressure Gradient Effects on Transition Location over Axisymmetric Bodies at Incidence in Supersonic Flow: Progress Report of JAXA-NASA Joint Research Project on Supersonic Boundary Layer Transition Part 2
MLA
Choudhari, Meelan, et al. “Pressure Gradient Effects on Transition Location over Axisymmetric Bodies at Incidence in Supersonic Flow: Progress Report of JAXA-NASA Joint Research Project on Supersonic Boundary Layer Transition Part 2.” 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report, Sept. 2017, pp. 1–49. EBSCOhost, widgets.ebscohost.com/prod/customlink/proxify/proxify.php?count=1&encode=0&proxy=&find_1=&replace_1=&target=https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&scope=site&db=edsair&AN=edsair.jairo.........5befd17feda2fcad41255b97e300a595&authtype=sso&custid=ns315887.
APA
Choudhari, M., Li, F., Chang, C., White, J., Tokugawa, N., Ueda, Y., Ishikawa, H., & Fujii, K. (2017). Pressure Gradient Effects on Transition Location over Axisymmetric Bodies at Incidence in Supersonic Flow: Progress Report of JAXA-NASA Joint Research Project on Supersonic Boundary Layer Transition Part 2. 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report, 1–49.
Chicago
Choudhari, Meelan, Fei Li, ChauLyan Chang, Jeffery White, Naoko Tokugawa, Yoshine Ueda, Hiroaki Ishikawa, and Keisuke Fujii. 2017. “Pressure Gradient Effects on Transition Location over Axisymmetric Bodies at Incidence in Supersonic Flow: Progress Report of JAXA-NASA Joint Research Project on Supersonic Boundary Layer Transition Part 2.” 宇宙航空研究開発機構研究開発報告 = JAXA Research and Development Report, September, 1–49. http://widgets.ebscohost.com/prod/customlink/proxify/proxify.php?count=1&encode=0&proxy=&find_1=&replace_1=&target=https://search.ebscohost.com/login.aspx?direct=true&site=eds-live&scope=site&db=edsair&AN=edsair.jairo.........5befd17feda2fcad41255b97e300a595&authtype=sso&custid=ns315887.