Transactions of the Japan Society for Aeronautical and Space Sciences

• 資料種別: 雑誌
• タイトル: Transactions of the Japan Society for Aeronautical and Space Sciences
• 巻次・部編番号: 53(179)-53(185/186):2010.5-2011.11
• 著者標目: 日本航空宇宙学会 ニホン コウクウ ウチュウ ガッカイ ( 00294140 )典拠
• 出版事項: Tokyo : Japan Society for Aeronautical and Space Sciences
• 出版年月日等: 2010-2011
• 出版年（W3CDTF）: 2010-2011
• 刊行巻次・年月次: v. 1, no. 1 (1958)-v. 58, no. 2 (Mar. 2015)
• 大きさ: 30cm
• 並列タイトル等: Transactions of the Japan Society of Aeronautical Engineering
• ISSN（掲載誌）: 0549-3811
• ISSN-L（掲載誌）: 0549-3811
• 出版地（国名コード）: JP
• 本文の言語コード: eng
• NDLC: ZN25
• 一般注記: Description based on the latest issue; Frequency varies; Title from coner; Title: Transactions of the Japan Society of Aeronautical Engineering (no. 1)
• 所蔵機関: 国立国会図書館
• 請求記号: Z53-M236
• 連携機関・データベース: 国立国会図書館 : 国立国会図書館蔵書; https://ndlsearch.ndl.go.jp
• 書誌ID（NDLBibID）: 000000126527; http://id.ndl.go.jp/bib/000000126527
• 目録規則: 日本目録規則1987年版改訂版

目次

Control of leakage flow by triple squealer configuration in axial flow turbine

Geometrical attitude determination algorithm based on vector measurements

Suppression of trailing-edge noise emitted by two-dimensional airfoils

Combustion characteristics of Bi-liquid swirl coaxial injectors with respect to a recess

An optimal guidance law applied to quadrotor using LQR method

Effect of Model Deformation on Aerodynamic Coefficients for the AGARD-B Wind Tunnel Model

Study on the Physical Mechanism of the Magnus Effect

Integrated Navigation for Flyback Reusable Booster Vehicles

Differential Game Guidance Law for Interceptor Missiles with a Time-varying Lateral Acceleration Limit

Robust Attitude Control and Compensation under Actuator Practical Restrictions

Fundamental performance of disk-shaped magnetohydrodynamics accelerator

Conservation-law approach to prediction of boundary layer transition

Disturbance observer based on multipoint feedback

Buckling modes and developable postbuckling modes of axially compressed short circular cylindrical shells

Identifying the ratio of aircraft applying SLOP by statistical modeling of lateral deviation

Multi-level of fidelity Multi-Disciplinary Design Optimization of small, solid-propellant launch vehicles

MHD analysis of magnetic diffusion effect on magneto plasma sail

Static and dynamic aerocharacteristics testing of strake-wing aerial vehicle in water tunnel

Designing integrated fuzzy guidance law for aerodynamic homing missiles using genetic algorithms

Numerical method of symplectic state transition matrix and application to fully perturbed Earth orbit

Induced drag characteristics based on wake surface integration for wing-in-ground effect

Effects of low Reynolds number on loss characteristics in transonic axial compressor

Comparison between hot and cold flow conditions of turbine cascade

Dynamic modeling and analysis of fixed-wing micro air vehicle

Analysis on thermal efficiency of non-compressor type pulse detonation turbine engines

Evaluation of longitudinal stability characteristics based on Irodov's criteria for wing-in-ground effect

Visualization of pressure field over rotating blades using pressure sensitive foil technique

Comparison study and sensitivity analysis of flight test techniques for air data position error correction in small aircraft

A new control scheme for satellite formation reconfiguration

Effects of inlet boundary layer thickness on characteristics of rotating stall in subsonic axial compressor

Formation control of small unmanned aerial vehicles using virtual leader and point-to-multipoint communication

Quantitative evaluation of ion kinetic effect in magnetic field inflation by the injection of a plasma jet

Advanced guidance scheme for lunar descent and landing from orbital speed conditions

Efficient calibration of the non-conservative force data from the space-borne accelerometers of the twin GRACE satellites

Vibration characteristics and thermal structural dynamic responses of a flexible rolled-up solar array