Youngjin JUN, Seongkyun IM

DOI Number: N/A

Conference number: HiSST-2024-278

A 6-inch high-enthalpy impulse test facility is constructed at Korea University. Impulse facilities, including an expansion tube, are capable of reproducing a wide range of high-enthalpy gas flows. While impulse facilities are renowned for their mechanical simplicity and cost-effectiveness, they have shorter test times. The primary objective of the expansion tube is to delve into the combustion characteristics of the scramjet combustor. In order to maximize test time, each section’s dimensions were meticulously optimized based on analytical solution. Subsequently, numerical simulations were carried out to verify the calculated test durations and conditions and assess the expansion tube’s performance. The facility was then constructed in accordance with the design specifications.

Read the full paper here

Email
Print
LinkedIn
The paper above was part of  proceedings of a CEAS event and as such the author has signed a publication agreement to have their paper published in the repository. In the case this paper is found somewhere else CEAS always links to the other source.  CEAS takes great care in making the correct content available to the reader. If any mistakes are found  in the listings please contact us directly at papers@aerospacerepository.org and we will correct the listing promptly.  CEAS cannot be held liable either for mistakes in editorial or technical aspects, nor for omissions, nor for the correctness of the content. In particular, CEAS does not guarantee completeness or correctness of information contained in external websites which can be accessed via links from CEAS’s websites. Despite accurate research on the content of such linked external websites, CEAS cannot be held liable for their content. Only the content providers of such external sites are liable for their content. Should you notice any mistake in technical or editorial aspects of the CEAS site, please do not hesitate to inform us.