検索結果 55 件
記録メディア記事
国立国会図書館全国の図書館
- 件名Mar Exploration Airplane CFD
- 並列タイトル等（連結）Decomposition for the aerodynamic analysis of Mars Exploration Airplane
- 並列タイトル等Decomposition for the aerodynamic analysis of Mars Exploration Airplane
記事
全国の図書館
- 要約等...s Conference / the 37th Aerospace......ts. However if there is a gas atmosphere around the planet, unmanned airplanes could provide...... detailed data of the planet surface......ept for a Mars airplane, and the preliminary analysis of the characteristic......as introduced. The new concept is called the “Wing-Tip-Chained” airplanes, and consist of multiple small airplanes joined together at the wing tips by r...... By connecting the wing tips and ......several) large airplanes with a high aspect ratio, the total induced ......hus, expanding the possible explo...... by increasing the efficiency of the flight. In order to clari...
- 並列タイトル等（連結）Preliminary Analysis of the Aerodynamic Ch......light Dynamics of Wing-Tip-Chained Airplanes
- 並列タイトル等Preliminary Analysis of the Aerodynamic Ch......light Dynamics of Wing-Tip-Chained Airplanes
デジタル記事
全国の図書館
- 一般注記...s Conference / the 37th Aerospace......ts. However if there is a gas atmosphere around the planet, unmanned airplanes could provide...... detailed data of the planet surface......ept for a Mars airplane, and the preliminary analysis of the characteristic......as introduced. The new concept is called the “Wing-Tip-Chained” airplanes, and consist of multiple small airplanes joined together at the wing tips by r...... By connecting the wing tips and ......several) large airplanes with a high aspect ratio, the total induced ......hus, expanding the possible explo...... by increasing the efficiency of the flight. In order to clari...
- 並列タイトル等（連結）Preliminary Analysis of the Aerodynamic Ch......light Dynamics of Wing-Tip-Chained Airplanes
- 並列タイトル等Preliminary Analysis of the Aerodynamic Ch......light Dynamics of Wing-Tip-Chained Airplanes
紙記事
国立国会図書館全国の図書館
- 並列タイトル等（連結）The aerodynamic characteristics of three dimensional wings for model airplanes
- 並列タイトル等The aerodynamic characteristics of three dimensional wings for model airplanes
デジタル記事
全国の図書館
- 要約等<jats:p>The main objective of this study is ......nt derivatives of aircraft attit......l flights. Out of these, the SNN multi-laye......, in which, in the forward propagation period, the time of output spikes ......ations instead of detection by t......ional methods. The phase of propagation of errors backward uses the step-by-step c......lation instead of the conventional g...... study enables the identification of aerodynamic co......culation time. The identification...... compared with the results when using the Radial Basis F......twork to prove the algorithm efficiency.</jats:p...
- 参照...e Map Analysis of Radar and Multispectral Image...
- 出版者（掲載誌）...ietnam Academy of Science and Technology (Publi...
紙規格・テクニカルリポート類
国立国会図書館
- 並列タイトル等（連結）AIAA applied aerodynamics conference. 20th. St. Louis, ...
- 並列タイトル等AIAA applied aerodynamics conference. 20th. St. Louis, ...
紙記事
国立国会図書館全国の図書館
- 並列タイトル等（連結）...iko HASHIMOTO, The Birth of Airplane and the Formation of Aerodynamic Research : The Origin of National Resea......nt, University of Tokyo Press, 2012
- 並列タイトル等...iko HASHIMOTO, The Birth of Airplane and the Formation of Aerodynamic Research : The Origin of National Resea......nt, University of Tokyo Press, 2012
デジタル記事
全国の図書館
- 要約等...s characterise the architecture of most new elect...... air mobility. The aerodynamic in......represents one of the key phenomena ......t characterise the flow field and performance of these novel aircra......onfigurations. The present article describes the main results of a wind tunnel ......to investigate the flow features ......e performed in the wake of two co-rotatin......configuration. The three-dimensio...... insights into the flow physics of the interacting pr......cular focus on the interactional effects on the trajectory of the tip vortices and the wake topology ......t cruise speed of eVTOLs in urban areas.</jats:...
- 参照Flight simulation from takeoff to yawing of eVTOL airplane with coaxial propellers by fl...
紙記事
国立国会図書館全国の図書館
- 並列タイトル等（連結）Aerodynamic characteristics of the wing for insect-size model airplane
- 並列タイトル等Aerodynamic characteristics of the wing for insect-size model airplane
紙デジタル記事
国立国会図書館全国の図書館
- 件名Database Aerodynamics Supersonic Transport
- 並列タイトル等（連結）Aerodynamic database of the super-sonic experimental airplane (NEXST-1) in JAXA
- 並列タイトル等Aerodynamic database of the super-sonic experimental airplane (NEXST-1) in JAXA
デジタル記事
全国の図書館
- 一般注記...apan As a part of the NAL's scaled s......c experimental airplane program to est......ntional linear theory. Then, the CFD and a supe......used to refine the wing geometry ......a design point of M = 2 and CL =...... By making use of the inverse method...... upper surface of the wing was desig......on designed by the linear theory to reduce a......pressure drag. The designed new w......tion drag than the initial geometry. Finally, the CFD analysis w...... to be used in the design. 資料番号: AA0063609010 レポ...
記事
全国の図書館
- 要約等...apan As a part of the NAL's scaled s......c experimental airplane program to est......ntional linear theory. Then, the CFD and a supe......used to refine the wing geometry ......a design point of M = 2 and CL =...... By making use of the inverse method...... upper surface of the wing was desig......on designed by the linear theory to reduce a......pressure drag. The designed new w......tion drag than the initial geometry. Finally, the CFD analysis w...... to be used in the design. 資料番号: AA0063609010 レポ...
デジタル記事
全国の図書館
- 一般注記...eration SST in the National Exper......e applied into the aerodynamic design of the unmanned and s......c experimental airplane with no propul......led 'NEXST-1'. These concepts consisted of arrow planform......ssure drag and the last one was o......friction drag. The aerodynamic design of the NEXST-1 airplane was conducted ......itatively. So, the flight test of the NEXST-1 airplane was expected t......ings. Finally, the effect on applying the NEXST-1 aerody......echnology into the design of a real size SS......y, improvement of about 13 % of the L/D of the real size SST ......comparing with the L/D of a Concorde-like config...
- 並列タイトル等（連結）Aerodynamic design of the NEXST-1 airplane
- 並列タイトル等Aerodynamic design of the NEXST-1 airplane
マイクロ図書
国立国会図書館
- 件名...tured grids (Mathematics) Euler equations of motion Mathematical models Aerodynamic cha...
記事
全国の図書館
- 要約等...eration SST in the National Exper......e applied into the aerodynamic design of the unmanned and s......c experimental airplane with no propul......led 'NEXST-1'. These concepts consisted of arrow planform......ssure drag and the last one was o......friction drag. The aerodynamic design of the NEXST-1 airplane was conducted ......itatively. So, the flight test of the NEXST-1 airplane was expected t......ings. Finally, the effect on applying the NEXST-1 aerody......echnology into the design of a real size SS......y, improvement of about 13 % of the L/D of the real size SST ......comparing with the L/D of a Concorde-like config...
- 並列タイトル等（連結）Aerodynamic design of the NEXST-1 airplane
- 並列タイトル等Aerodynamic design of the NEXST-1 airplane
デジタル記事
全国の図書館
- 一般注記...ogy for Design of Next Generatio......c experimental airplane to establish the technological basis for the development of the next generatio......d experimental airplane is being developed for the first experime......light in 2002. The airplane is launched by......booster. After the rocket-booster is separated, the airplane starts the measurement fl......de 18.5 km. In the aerodynamic design of the experimental airplane, Mitsubishi He......) is in charge of the overall design......inly conducted the wing and wing-......on design with their sophisticate......also in charge of the launch configu......mic design. In the MHI design work, wind tunnel ...
記事
全国の図書館
- 要約等...ogy for Design of Next Generatio......c experimental airplane to establish the technological basis for the development of the next generatio......d experimental airplane is being developed for the first experime......light in 2002. The airplane is launched by......booster. After the rocket-booster is separated, the airplane starts the measurement fl......de 18.5 km. In the aerodynamic design of the experimental airplane, Mitsubishi He......) is in charge of the overall design......inly conducted the wing and wing-......on design with their sophisticate......also in charge of the launch configu......mic design. In the MHI design work, wind tunnel ...
デジタル記事
全国の図書館
- 件名Database, Aerodynamics, Supersonic Transport
- 一般注記...e system named the NEXST-DB was c...... contribute on the aerospace rese......apan. A number of aerodynamic data on the supersonic experimental airplane (NEXST-1) can ......accumulated by the NEXST project. Three kinds of data of the pressure distr......ere carried on the NEXST-DB. These aerodynamic ...... obtained from the flight test, C......nnel tests. Furthermore, the geometry data of the NEXST-1 and the grid data for ......lso carried on the NEXST-DB. Thos......an download on the website. 形態: カラー図版あり 資料番号: AA...
- 並列タイトル等（連結）Aerodynamic database of the supersonic experimental airplane (NEXST-1) in JAXA
記事
全国の図書館
- 要約等...e system named the NEXST-DB was c...... contribute on the aerospace rese......apan. A number of aerodynamic data on the supersonic experimental airplane (NEXST-1) can ......accumulated by the NEXST project. Three kinds of data of the pressure distr......ere carried on the NEXST-DB. These aerodynamic ...... obtained from the flight test, C......nnel tests. Furthermore, the geometry data of the NEXST-1 and the grid data for ......lso carried on the NEXST-DB. Thos......an download on the website. 形態: カラー図版あり 資料番号: AA...
- 件名Database, Aerodynamics, Supersonic Transport
- 並列タイトル等（連結）Aerodynamic database of the supersonic experimental airplane (NEXST-1) in JAXA
記事
全国の図書館
- 要約等...XA to validate the aerodynamic de......ign technology of the supersonic tra......dynamic forces of the supersonic experimental airplane (NEXST-1) were obtained by the flight test. F......comparing with the CFD analysis. ...... observed with the flight test results and the CFD results. The validity of the drag reduction......confirmed from the flight test. 形態: カラー図版あり 資料番号...
- 並列タイトル等（連結）... distributions of the supersonic experimental airplane (NEXST-1) on the flight test
- 並列タイトル等... distributions of the supersonic experimental airplane (NEXST-1) on the flight test