Eduard B. Vasilevsky , Ivan V. Ezhov , Pavel V. Chuvakhov

DOI Number XXX-YYY-ZZZ

Conference Number HiSST 2018_9001039

The aircraft, designed for long-term hypersonic flight, should have possibly small blunting of the leading edges. This is necessary to reduce the external resistance of the apparatus, as well as internal losses of the total pressure in the air intake. Reducing the blunting radius of the leading edges is prevented by overheating of the structure due to aerodynamic heating. One promising method for thermal protection of the leading edges with a small blunting radius is the blowing of the cooling gas through a gap located on the critical line of blunt wedge. In the following work several applications of this method are presented.

Read the full paper >

In Categories: HiSST 2018, Materials and Structures, Thermal and Energy Management Systems, Thermal Protection Systems, Thermal Protection Systems
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.