Drag Reduction on the Basis of the Area Rule of the Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology

التفاصيل البيبلوغرافية
العنوان: Drag Reduction on the Basis of the Area Rule of the Small-scale Supersonic Flight Experiment Vehicle Being Developed at Muroran Institute of Technology
المؤلفون: 山﨑, 優樹, YAMAZAKI, Yuki, ヤマザキ, ユウキ, 溝端, 一秀, ミゾバタ, カズヒデ, MIZOBATA, Kazuhide, 東野, 和幸, ヒガシノ, カズユキ, HIGASHINO, Kazuyuki
بيانات النشر: JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
سنة النشر: 2019
المجموعة: Muroran Institute of Technology Academic Resources Archive / 室蘭工業大学学術資源アーカイブ
مصطلحات موضوعية: Supersonic, Drag Reduction, Area Rule, Wave Drag Analysis, Wind Tunnel Test
Time: 538
الوصف: application/pdf ; A small-scale supersonic flight experiment vehicle (OWASHI) is being developed at Muroran Institute of Technology as a flying testbed for verification of innovative technologies for high speed atmospheric flights which are essential to next-generation aerospace transportation systems. The second-generation configuration M2011 of the vehicle with a single Air Turbo Ramjet Gas-generator-cycle (ATR-GG) engine has been proposed. Its transonic thrust margin has been predicted to be insufficient, therefore drag reduction in the transonic regime is quite crucial for attainability of supersonic flights. In this study, we propose configuration modifications for drag reduction on the basis of the so-called area rule, and assess their effects through wave drag analysis, wind tunnel tests, and CFD analysis. As a result, the area-rule-based configurations have less drag than the baseline configuration M2011. However, the effects of the proposed bottleneck on the fuselage below the main wing are smaller than predicted. It would be caused by the drag due to separation and shocks around the bottleneck. It is necessary to redesign the area-rule-based bottleneck to be smoother. ; journal article
نوع الوثيقة: other/unknown material
وصف الملف: application/pdf
اللغة: English
تدمد: 1884-0485
Relation: 130007607485; TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN; 17; 127; 133; https://muroran-it.repo.nii.ac.jp/record/10158/files/TJSASS_17_2_127_133.pdf
الاتاحة: https://muroran-it.repo.nii.ac.jp/record/10158/files/TJSASS_17_2_127_133.pdf
Rights: © 2019 JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES ; open access
رقم الانضمام: edsbas.D5650DE4
قاعدة البيانات: BASE