JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
titleソニックブーム推算手法検証風洞試験における主翼空力弾性変形効果
Other TitleAeroelastic Deformation Effects of the Main Wing in the Wind-tunnel Test for Validating Sonic-boom Prediction Methods
Author(jpn)近藤, 賢; 上野, 篤史; 平野, 義鎮; 野口, 正芳; 牧野, 好和; 石川, 敬掲
Author(eng)Kondo, Satoshi; Ueno, Atsushi; Hirano, Yoshiyasu; Noguchi, Masayoshi; Makino, Yoshikazu; Ishikawa, Hiroaki
Author Affiliation(jpn)株式会社菱友システムズ; 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 宇宙航空研究開発機構(JAXA); 株式会社エイ・エス・アイ総研
Author Affiliation(eng)Ryoyu Systems Co., Ltd.; Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Japan Aerospace Exploration Agency (JAXA); Advanced Science & Intelligence Research Institute (ASIRI)
Issue Date2017-12-27
Publisher宇宙航空研究開発機構(JAXA)
Japan Aerospace Exploration Agency (JAXA)
Publication title宇宙航空研究開発機構特別資: 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム論文集
JAXA Special Publication: Proceedings of the 49th Fluid Dynamics Conference / the 35th Aerospace Numerical Simulation Symposium
VolumeJAXA-SP-17-004
Start page39
End page45
Publication date2017-12-27
Languagejpn
eng
AbstractThe demand of Supersonic Transport (SST) is increasing globally. Some companies have announced their program for developing civil supersonic airplanes and the International Civil Aviation Organization (ICAO) has started developing the sonic boom standard for supersonic overland flight. Second AIAA Sonic Boom Prediction Workshop (SBPW2) has been held in January 2017 to assess the state of the art for predicting sonic boom. Japan Aerospace Exploration Agency (JAXA) designed a simple low boom configuration named 'JAXA Wing Body (JWB)' and provided it to the workshop for one of the test cases of SBPW2. For the validation of sonic boom prediction method, the supersonic wind-tunnel test of the JWB model was carried out at JAXA's supersonic wind-tunnel. This paper reports the development of an aeroelastic deforming estimation tool of the main wing in wind tunnel test and the results of CFD analysis for prediction of near-field sonic boom signature with aeroelastic deformation effects.
Description会議情報: 第49回流体力学講演会/第35回航空宇宙数値シミュレーション技術シンポジウム (2017年6月28日-34日. 国際オリンピック記念青少年総合センター), 渋谷区, 東京
形態: カラー図版あり
Meeting Information: 49th Fluid Dynamics Conference /the 35th Aerospace Numerical Simulation Symposium (June 28-30, 2017. National Olympics Memorial Youth Center), Shibuya-ku, Tokyo, Japan
Physical characteristics: Original contains color illustrations
Document TypeConference Paper
JAXA Category特別資料
NASA Subject CategoryFluid Mechanics and Thermodynamics
ISSN(online)2433-2232
SHI-NOAA1730011004
Report NoJAXA-SP-17-004
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/865284


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