Zobrazeno 1 - 10
of 19
pro vyhledávání: '"Sandy Tirtey"'
Publikováno v:
Journal of Spacecraft and Rockets. 52:684-696
This paper reports on the methodology and results of a weak-coupled aerothermal–structural analysis on the ascent phase of the SCRAMSPACE Mach 8 scramjet flight experiment. This vehicle was essenti...
Publikováno v:
Experiments in Fluids. 50:407-418
The flow-field structure in the vicinity and in the wake of an isolated 3D roughness element has been studied. Different experimental techniques have been coupled and supported by CFD simulation for a good understanding of the flow-field topology. Th
This paper presents the results from a coupled numerical and experimental investigation of the flow and combustion characteristics of an inlet-fuelled scramjet engine. Testing of the model was conducted in the T4 shock tunnel at the University of Que
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4aab7890b3e8e3e01bb58de406b75221
https://doi.org/10.2514/mhyp12
https://doi.org/10.2514/mhyp12
Publikováno v:
Scopus-Elsevier
The design of a navigation processor for the SCRAMSPACE 1 hypersonic flight experiment is detailed. Two cascaded extended Kalman filters provide a fusion of gyroscope, accelerometer, magnetometer, GPS and aerodynamic database sources for vehicle stat
Autor:
Bianca R. Capra, Laurie Brown, Russell Boyce, Paul A. van Staden, Igor Dimitrijevic, Sandy Tirtey, Michael A. Creagh
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
The design activities of the development of the SCRAMSPACE I scramjet-powered free-flight experiment are described in this paper. The objectives of this flight are first described together with the definition of the primary, secondary and tertiary ex
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
The design and simulation of an attitude control strategy using four cold gas thrusters is detailed. The system is designed to re-orient the hypersonic experimental vehicle SCRAMSPACE 1 outside the atmosphere so that on re-entry at 80 km altitude, it
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
A 2D numerical investigation was undertaken utilising transient, time-accurate, RANS computational fluid dynamics, with the aim of investigating the influence of viscous and unsteady effects when attempting to start a hypersonic scramjet inlet. A var
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
The free-flying SCRAMSPACE I Mach 8 hypersonic flight experiment will be launched using a two-stage sounding rocket motor system (RMS) from the Andoya Test Range in Norway in June 2013. The vehicle will reach an altitude of approximately 100km before
Publikováno v:
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
The results for the internal flowpath at zero degrees angle of attack for the 'SCRAMSPACE I' axially-symmetric, free-flying, supersonic combustion ramjet (scramjet) hypersonic flight experiment are presented. The results demonstrate the performance o
Publikováno v:
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Scramjet-based launch systems offer considerable promise for safe, reliable and economical access to space. Through both flight and ground tests, leveraging Australia's world leadership in scramjet R and D, the SCRAMSPACE project will answer key scie