Zobrazeno 1 - 10
of 557
pro vyhledávání: '"thrust vector control"'
Autor:
Atik, Nuri1, Gürkan, Serkan2 natik@msu.edu.tr
Publikováno v:
Gazi Journal of Engineering Sciences (GJES) / Gazi Mühendislik Bilimleri Dergisi. agu2023, Vol. 9 Issue 2, p334-346. 13p.
Akademický článek
Tento výsledek nelze pro nepřihlášené uživatele zobrazit.
K zobrazení výsledku je třeba se přihlásit.
K zobrazení výsledku je třeba se přihlásit.
Autor:
Tanveer, Ahsan, Ahmad, Sarvat Mushtaq
Publikováno v:
Engineering Proceedings; 2023, Vol. 56, p90, 7p
Publikováno v:
Chemical Engineering Research & Design: Transactions of the Institution of Chemical Engineers Part A. Jan2017, Vol. 117, p533-541. 9p.
Autor:
Acampora Prado, Igor Afonso1 igoracampora@gmail.com, dos Santos, Davi Antônio1
Publikováno v:
Journal of Aerospace Technology & Management. Jan-Mar2017, Vol. 9 Issue 1, p116-128. 13p.
Autor:
Jan Sieder-Katzmann, Martin Propst, Ralf H. Stark, Dirk Schneider, Stephan General, Martin Tajmar, Christian Bach
Publikováno v:
Aerospace, Vol 11, Iss 7, p 507 (2024)
A cold-gas test campaign has been conducted at the DLR’s P6.2 test bench in Lampoldshausen, with the objective of investigating the linear aerospike nozzle flow in interaction with secondary injection thrust vector control (SITVC). In this campaign
Externí odkaz:
https://doaj.org/article/247ed885979145fba4704bc4ccf292af
Autor:
ŽIVKOVIĆ, Saša Ž.1 sasavite@yahoo.com, MILINOVIĆ, Momčilo M.2, STEFANOVIĆ, Predrag Lj.3, PAVLOVIĆ, Pavle B.3, GLIGORIJEVIĆ, Nikola I.1,4
Publikováno v:
Thermal Science. 2016 Supplement, Vol. 20, pS175-S286. 12p.
Publikováno v:
Journal of Applied Fluid Mechanics, Vol 16, Iss 4, Pp 765-777 (2023)
This article studies the aerodynamic performance of a novel bypass shock-induced thrust vector nozzle. An arc-shaped bypass is innovatively designed to optimize nozzle performance and equips a variable shrinkage part. The nozzle performance is invest
Externí odkaz:
https://doaj.org/article/5fa3b1aaabd940bebf9e3c50331f4513
Publikováno v:
Fluid Dynamics. Mar2014, Vol. 49 Issue 2, p288-297. 10p. 1 Diagram, 6 Graphs.
Autor:
Li, Li1, Saito, Tsutomu2
Publikováno v:
International Journal of Aerospace Innovations. Dec2013, Vol. 5 Issue 3/4, p51-60. 10p.