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Takashi Tani

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Publication

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Journal of The Japan Society for Aeronautical and Space Sciences | 1957

A Method for Solving the Second Order Problems of Axially Symmetric Supersonic Flow

Takashi Tani

The second order equation of perturbation stream function for the axially symmetric irrotational compressible flow is studied by assuming that the axial component of perturbation velocity is the same order as the radial velocity. In some cases the equation can be solved in closed form. Generalized conical flow is represented by elementary integral.

Transactions of the Japan Society of Mechanical Engineers. B | 1987

NUMERICAL INVESTIGATION OF FLOW AROUND TWO RECTANGULAR CYLINDERS BY A DISCRETE VORTEX METHOD.

Norio Arai; Katsuhiko Taguchi; Takashi Tani

Archive | 1990

Active control of vortex shedding frequency by a splitter plate

Norio Arai; Masatomo Komatsu; Takashi Tani

Journal of The Japan Society for Aeronautical and Space Sciences | 1987

Subsonic flow region on blunted cones in supersonic flow.

Takashi Tani; Norio Arai; Koetsu Takehana; Hideo Sekine; Naoki Hirose

JSME international journal : bulletin of the JSME | 1987

Numerical Investigation of Flow Around Two Rectangular Cylinders by a Discrete Vortex Method : Series B : Fluid Engineering Heat Transfer Combustion, Power Thermophysical Properties

Norio Arai; Katsuhiko Taguchi; Takashi Tani

Archive | 1981

Surface Temperature Distribution Effects on Stable Shape of Ablating Blunt Bodies

紀夫 新井; 桂一 辛島; Norio Arai; Takashi Tani; Keiichi Karashima

Journal of The Japan Society for Aeronautical and Space Sciences | 1966

Aerodynamics of the NAL-16 rocket

Takashi Tani

Journal of The Japan Society for Aeronautical and Space Sciences | 1965

Aerodynamic Characteristics of Vehicles Traveling at Hypervelocities

Takashi Tani

Journal of The Japan Society for Aeronautical and Space Sciences | 1964

Preliminary Tests of Mach Number Effect on Static Stability of Rocket Vehicles

Takashi Tani; Nobutoshi Hara; Hideo Sekine

Journal of The Japan Society for Aeronautical and Space Sciences | 1963

An Investigation of the Lift, Drag, and Pitching Moment Characteristics of AGARD Calibration Model B in N.A.L. 1m×1m Supersonic Blowdown Wind Tunnel.

Hiroharu Takagi; Takashi Tani; Hideo Saito; Kiyoshi Arai

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Norio Arai

Tokyo University of Agriculture and Technology

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Akira Takano

University of Tokyo

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Tomijiro Moriya

University of Tokyo

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