Results 41 to 50 of about 4,462 (234)
Investigation of the Flow In Cold Condition at the Exit of a Supersonic Combustor Test Bench [PDF]
Journal of Aerospace Technology and Management, 2020 For studies of hypersonic flows and supersonic combustion in ground test facilities, three devices can be used as ram accelerators, shock tunnels and supersonic combustor test benches.
Jefte da Silva Guimarães +3 more
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Medium independent jet (MI-Jet) engine
Propulsion and Power Research, 2020 MI-Jet or medium independent jet engine is a new conceptual design which can be used in any gaseous atmosphere or in any planets with an ISP greater than that of the existing rocket engines.
Prajith Kumar K P, Aravind Vaidyanathan
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, 2011 In this paper, we present the results of an extensive measurement campaign to investigate the effect of external and internal sidewall compression as well as different contraction ratios on the performance of the flowfield of a scramjet inlet ...
Ali Gülhan +3 more
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The Scientific World Journal, 2014 The influence of the in-stream pylon and strut on the performance of scramjet combustor was experimentally and numerically investigated. The experiments were conducted with a direct-connect supersonic model combustor equipped with multiple cavities.
Hao Ouyang, Weidong Liu, Mingbo Sun
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, 2012 We conducted an extensive experimental examination of the operational behavior of a three-dimensional scramjet inlet featuring a movable cowl to adapt the internal contraction according to the respective operation conditions.
Hohn, Oliver +3 more
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International Journal of Applied Ceramic Technology, Volume 23, Issue 1, February 2026.Abstract Novel compositionally complex borides, (Hf,Zr,Nb,Ti)B2 and (Hf,Zr,Nb,Ti)B2‒LaB6, were fabricated using spark plasma sintering process. (Hf,Zr,Nb,Ti)B2‒LaB6 exhibits a dual‐phase microstructure, in which (Hf,Zr,Nb,Ti)B2 is a primary phase with the hexagonal structure and LaB6 is a secondary phase with a cubic structure.
Xin Chen +8 more
wiley +1 more source
Thrust vector control systems in scramjet propelled aircraft
, 2023 openFin dal volo inaugurale dei fratelli Wright, continue innovazioni tecnologiche hanno caratterizzato il panorama aeronautico e spaziale. Effettuare il trasporto di merci e passeggeri ad alta velocità e ottenere un accesso economico allo spazio sono ...
CIAMPA', DIEGO
core
Chemistry–Methods, Volume 6, Issue 1, January 2026.A high‐pressure shock‐tube facility is developed to investigate high‐temperature chemical‐kinetics for next‐generation combustion systems. The design enables extended test times and integrates multiple optical diagnostics for time‐resolved species detection.
Sulaiman A. Alturaifi +8 more
wiley +1 more source
Multilateral‐Jets Interaction on Hypersonic Missiles: A Numerical Investigation
International Journal of Aerospace Engineering, Volume 2026, Issue 1, 2026.This paper numerically investigates flow field interaction and aerodynamic interference characteristics of multilateral‐jets on hypersonic missiles. Three‐dimensional compressible RANS equations coupled with the SST k‐ω turbulence model are solved using the finite volume method.
Zhao Sun +3 more
wiley +1 more source
Numerical Study of Disturbance Resistance of Oblique Detonation Waves
International Journal of Aerospace Engineering, 2020 The stability of oblique detonation waves (ODWs) is a fundamental problem, and resistance of ODWs against disturbances is crucial for oblique detonation engines in high-speed propulsion. In this work, numerical studies on ODW stability in disturbed flows
Yu Liu, Baoguo Xiao, Lan Wang, Chao Wang
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