Research of Wing-in-Ground Effect Craft by Radio Control Models
Research of Wing-in-Ground Effect Craft by Radio Control Models
批准号:
62550047
负责人:
KUBO Syozo
金额:
$1.28万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for General Scientific Research (C)
财政年份:
1987
资助国家:
日本
项目状态:
已结题
起止时间:
1987 至 1989
中文摘要
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英文摘要
Flying tests of radio controlled models of Wing-in-Ground Effect (WIG) craft were conducted using 3 models of TN-1,2 and -3 at Tottori University, and other 3 models of NT-1,2 and MNT-3 at Nagoya University.TN-1 had a Lippisch wing with a canard, which deflrct slip stream of a propeller mounted in front of its nose and drived by a gas engine. NT-1 had an ordinary flying-boat type. Its wing was a modified Lippisch wing, whose leading edges were cut out to introduce slip streams of two propellers mounted in front of its nose and drived by two electric motors. These two types of models revealed that they were suitable for a high speed and high efficiency craft. From this time, weight of research effort was put on the development of a low speed and small craft at Tottori University. On the other hand, at Nagoya University, effort was continued to develop a high efficiency craft. TN-2 had a ram wing, which could achieve a low wing loading and was suitable for a low speed craft. Wing of NT-2 … More was rectilinear instead of a Lippisch wing to maximize the effect of power augmented lift (PAR). TN-2 had satisfactory performance except the tendency of pitch up. To control pitch up, TN-3 was designed and constructed. Two electric motors of NT- 2 were not enough powerful for its model size. A new model MNT-3 was designed with a gas engine. These last two models achieved constant low altitude flight above water surface.During this research project, investigators in Tottori University had a chance to advice another project of manned model of WIG. A 1-seater and a 2-seater were developed in success. They are now making effort to develop a production model. At the same time, investigators in Nagoya University also advised a project of a manned model of PAR-WIG. This model succeeded to a continuous jump. They obtained many valuable data of PAR-WIG development.From these results, we find out that one of important problem is pitching stability for the practical use of WIG. We will study the problem by making use of numerical simulation. Less
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Ando, S.: "A New Concept of Surface Aircraft (Power-Augmented Ram Wing) (in Japanese)" J.JAPAN SOC. AERO. SPACE SCI.35-397. 91-101 (1987)
Ando, S.:“地面飞机的新概念(动力增强冲压翼)(日语)”J.JAPAN SOC。
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Kawamura,T.and Kubo,S.: "Numerical Simulation of Wing in Ground Effect" A Collection of Technical Papers of Int.Symp.on Comput.Fluid Dynamics Nagoya. 1037-1042 (1989)
Kawamura,T. 和 Kubo,S.:“地面效应中机翼的数值模拟”Int.Symp.on Comput.Fluid Dynamics Nagoya 技术论文集。
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Kawamura, T. and Kubo, S.: "Numerical Simulation of Wing in Ground Effect" A COLL. TECH. PAPERS INT. SYMP. COMPUT. FLUID DYN. NAGOYA,, 1037-1042, 1989.
Kawamura, T. 和 Kubo, S.:“地面效应中机翼的数值模拟”COLL。
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安東茂典: "水面飛行機(Power-Augmented Ram Wing)の一構想," 日本航空宇宙学会誌. 35. 91-101 (1987)
Shigenori Ando:“动力增强冲压翼的概念”,日本航空航天学会杂志 35. 91-101 (1987)。
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河村哲也,久保昇三: "地面効果翼機まわりの流れの水値シミュレ-ション" 航空宇宙技術研究所特別資料. SP-9. 223-227 (1988)
Tetsuya Kawamura,Shozo Kubo:“地效翼飞机周围的水值模拟”航空航天技术研究所特殊材料。223-227(1988)。
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共 14 条
Basic Development of Wing-In-Surface-Effect Ship of a New Configuration with High Seaworthiness
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批准号:14205145
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项目类别:Grant-in-Aid for Scientific Research (A)
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资助金额:$23.88万
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财政年份:2002
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负责人:KUBO Syozo
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依托单位:
BASIC RESEARCH ON NOISE REDUCTION OF HOVERCRAFT
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批准号:12650902
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$1.79万
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财政年份:2000
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负责人:KUBO Syozo
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依托单位:
Performance Analysis of a Wing-In-Surface-Effect Craft on the Basis of Extreme Ground Effect Theory
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批准号:09651014
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$2.18万
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财政年份:1997
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负责人:KUBO Syozo
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依托单位:
国内基金
海外基金
凋亡相关分子WIG-1在缺氧介导食管癌多药耐药中的作用及其分子机制的研究
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批准号:81071976
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项目类别:面上项目
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资助金额:33.0万元
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批准年份:2010
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负责人:郭伟
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依托单位: