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journal of aerospace science and technology
سال:2020 - دوره:13 - شماره:2
a simulation algorithm for staged combustion cycle liquid propellant rocket engines
- صفحه:85-91
analysis of torsional hysteresis behavior of shaft
- صفحه:67-72
conceptual design of aeroderivative industrial gas turbines
- صفحه:37-46
design of deterministic self-tuning regulators for the pitch angle of an aircraft
- صفحه:61-66
experimental study of the spray pattern of a non-newtonian gelled fluid using two impinging jets
- صفحه:125-134
investigating cooperative and non-cooperative interference elimination between aircraft using game theory
- صفحه:103-113
investigating the effects of noise and parameter changing on modeling of jet transport aircraft
- صفحه:47-52
multi-scale modeling for thermal conductivity analysis of epoxy nanocomposite - cnt
- صفحه:1-6
numerical and experimental analysis of ballistic behavior of ceramic-reinforced aluminum matrix composites plates
- صفحه:7-26
restricted three-body problem considering perturbations of oblate primaries
- صفحه:27-35
the strategy of using porous material in liquid fuel space propulsion injectors
- صفحه:73-84
two-phase cfd modeling of three- dimensional supercavitating flows
- صفحه:53-60
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