Results 101 to 110 of about 892,130 (360)

Fluid thrust control system [PDF]

, 1968
A pure fluid thrust control system is described for a pump-fed, regeneratively cooled liquid propellant rocket engine. A proportional fluid amplifier and a bistable fluid amplifier control overshoot in the starting of the engine and take it to a ...
Howell, W. L., Jansen, H. B., Lehmann, E. N.   +2 more
core   +1 more source

Structural dynamics of the large thrust liquid rocket engines [PDF]

, 2018
DaoQiong HUANG, Zhen Wang, Dahua Du
openalex   +1 more source

Preparing for Tomorrow's Teamwork: Insights From eSports on How Human Expertise Shapes Training Needs for AI‐Integrated Work

Journal of Organizational Behavior, EarlyView.
ABSTRACT As organizations increasingly adopt human‐AI teams (HATs), understanding how to enhance team performance is paramount. A crucially underexplored area for supporting HATs is training, particularly helping human teammates to work with these inorganic counterparts.
Caitlin M. Lancaster, Christopher Flathmann, Jennifer Hsu, Nathan J. McNeese, Thomas A. O'Neill, Eduardo Salas   +5 more
wiley   +1 more source

Dataset of the experimentally measured heat transfer in the throat region of liquid rocket engine thrust chambers. [PDF]

Data Brief, 2021
Pizzarelli M.
europepmc   +1 more source

Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines [PDF]

Fiber reinforced ceramic matrix composites (FRCMC) are emerging materials systems that offer potential for use in liquid rocket engines. Advantages of these materials in rocket engine turbomachinery include performance gain due to higher turbine inlet ...
Brockmeyer, Jerry W., Schnittgrund, Gary D.   +1 more
core   +1 more source

Cattaneo-Christov heat flux and entropy generation on hybrid nanofluid flow in a nozzle of rocket engine with melting heat transfer

Case Studies in Thermal Engineering, 2021
H. Waqas, Taseer Muhammad, Sobia Noreen, Umar Farooq, Metib Alghamdi   +4 more
semanticscholar   +1 more source

Nonlinear Combustion Instability in a Multi-Injector Rocket Engine

AIAA Journal, 2018
A computational study is presented of the nonlinear combustion instability of a multi-injector rocket engine.
J. Xiong
semanticscholar   +1 more source

Numerical Approach for the Estimation of Throat Heat Flux in Liquid Rocket Engines [PDF]

, 2020
Pierluigi Concio, Mario Tindaro Migliorino, Francesco Nasuti   +2 more
openalex   +1 more source

Setting the Record Straight: The Intellectual Legacy of H. Igor Ansoff (1918–2002)

Strategic Change, EarlyView.
ABSTRACT This study presents a comprehensive annotated bibliography of H. Igor Ansoff's intellectual contributions, addressing significant gaps in existing citation databases such as Scopus and Web of Science, which capture only 9 to 15 percent of his work.
Richard W. Puyt
wiley   +1 more source

Numerical Investigation on the Effect of Fuel-Rich Degree in the RBCC Engine under the Ejector Mode

International Journal of Aerospace Engineering
The ejector mode of the Rocket-Based Combined-Cycle (RBCC) engine is characterized by high fuel consumption. This study is aimed at investigating the influence of the rocket fuel-rich degree on the RBCC engine’s performance under the ejector mode ...
Yizhi Yao, Mingbo Sun, Menglei Li, Peibo Li, An Bin, Rui Gu, Jiaoru Wang, Feng Wei, Taiyu Wang, Jikai Chen   +9 more
doaj   +1 more source