Zobrazeno 1 - 4
of 4
pro vyhledávání: '"Nimesh, Dahal"'
Publikováno v:
Aerospace Science and Technology. 105:105954
The supersonic wind tunnel tests using a rigid parachute model were conducted for Mach numbers ranging from 2.0 to 3.0. The rigid model consists of suspension lines and a riser between the forebody and rear body, and the effect of these suspension li
Publikováno v:
平成30年度宇宙航行の力学シンポジウム = Symposium on Flight Mechanics and Astrodynamics: 2018.
平成30年度宇宙航行の力学シンポジウム(2018年12月10日-11日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県
Symposium on Flight Mechanics and Astrodynamics: 2018 (December 10-
Symposium on Flight Mechanics and Astrodynamics: 2018 (December 10-
Publikováno v:
22nd AIAA International Space Planes and Hypersonics Systems and Technologies Conference.
Publikováno v:
平成29年度宇宙航行の力学シンポジウム = Symposium on Flight Mechanics and Astrodynamics: 2017.
平成29年度宇宙航行の力学シンポジウム(2017年12月7日-8日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県
Symposium on Flight Mechanics and Astrodynamics: 2017 (December 7-8,
Symposium on Flight Mechanics and Astrodynamics: 2017 (December 7-8,