Zobrazeno 1 - 10
of 12
pro vyhledávání: '"Kevin G. Bowcutt"'
Publikováno v:
AIAA Propulsion and Energy 2021 Forum.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::79551cccbe4b4b756bf646219680fcf4
https://doi.org/10.2514/6.2021-3531
https://doi.org/10.2514/6.2021-3531
Autor:
Kevin G. Bowcutt, Troy Winfree, Christopher C. Huffman, Thomas J. Juliano, Matthew T. Lakebrink
Publikováno v:
Journal of Spacecraft and Rockets. 55:315-321
Numerical simulations were conducted to optimize the shape and wall-temperature distribution of the Notre Dame Mach 6 quiet tunnel nozzle. The design was optimized by minimizing the overall nozzle ...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::966d98cc8739ea727ea1db6073cd0e58
https://doi.org/10.2514/1.a33794
https://doi.org/10.2514/1.a33794
Autor:
Kevin G. Bowcutt
Publikováno v:
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::16c6c2baa980c5c6a25bccb2ed6d8fd6
https://doi.org/10.2514/6.2018-5373
https://doi.org/10.2514/6.2018-5373
Publikováno v:
Journal of Aircraft. 51:1973-1986
A general strategy is identified to compute the minimum fuel required for the ascent of a generic hypersonic vehicle that is propelled by a dual-mode ramjet–scramjet engine with hydrogen fuel. The study addresses the ascent of an accelerator vehicl
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d21d38bbb6d84278536319c0f5908c40
https://doi.org/10.2514/1.c032617
https://doi.org/10.2514/1.c032617
Publikováno v:
18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference.
The Hypersonic International Flight Research and Experimentation (HIFiRE) program is a joint effort between the United States Air Force Research Laboratory (AFRL) and the Australian Defence Science and Technology Organisation (DSTO). Boeing is an ind
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c7ea6151b92d798e95c571278a864ee5
https://doi.org/10.2514/6.2012-5842
https://doi.org/10.2514/6.2012-5842
Autor:
Kei Lau, Allan Paull, Thomas R. Smith, Eric Unger, Brandin Northrop, John Selmon, Douglas Dolvin, Luis Miranda, Ross Paull, Ron Mairs, Kevin G. Bowcutt, Todd Silvester, Hans Alesi
Publikováno v:
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
The Hypersonic International Flight Research and Experimentation (HIFiRE) program is a joint effort between the United States Air Force Research Laboratory (AFRL) and the Australian Defence Science and Technology Organisation (DSTO). Boeing is an ind
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::46c0119feff04f701f7b758210e646fe
https://doi.org/10.2514/6.2011-2275
https://doi.org/10.2514/6.2011-2275
Autor:
Kevin G. Bowcutt, John W. Livingston, Thomas R. Smith, Venkatraman Raghavan, Christopher Tarpley, Ajay P. Kothari
Publikováno v:
17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Several rocket boosted RBCC (Rocket-Based Combined Cycle) designs were created and analyzed for suitability for an access-to-space TSTO vehicle system. Level 1 analysis was performed that included vehicle closure, weight breakdown (to component level
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f42342b0ae3a9c484fc7a82061602831
https://doi.org/10.2514/6.2011-2338
https://doi.org/10.2514/6.2011-2338
Autor:
Christopher Tarpley, Ajay P. Kothari, John W. Livingston, Venkatraman Raghavan, Kevin G. Bowcutt, Thomas R. Smith
Publikováno v:
AIAA SPACE 2010 Conference & Exposition.
Several rocket boosted RBCC (Rocket-Based Combined Cycle) designs were created and analyzed for suitability for an access-to-space TSTO vehicle system. Level 1 analysis was performed that included vehicle closure, weight breakdown (to component level
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f3abfdc331764e980a6ba4ced5ecfc31
https://doi.org/10.2514/6.2010-8905
https://doi.org/10.2514/6.2010-8905
Publikováno v:
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1627fc83b8f3d342884ec0b429a0cac4
https://doi.org/10.2514/6.2008-2591
https://doi.org/10.2514/6.2008-2591
The objective of this effort is to modify an existing engineering code to provide fast prediction capabilities to assess the aerothermodynamic performance characteristics of advanced high speed configurations throughout a flight trajectory. The predi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::8822e2a3b817eb349627ac9782171874
https://doi.org/10.21236/ada455794
https://doi.org/10.21236/ada455794
