Swirling Flow Field inside a Hollow Turbine Shaft for an Internal Cooling Air System von Kishibe, Tadaharu, Kaji, Shojiro

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Study on the Swirling Flow Field in a Rotating Cylinder : Numerical Analysis von KISHIBE, Tadaharu, KAJI, Shojiro

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Study on the Swirling Flow Field in a Rotating Cylinder (2nd Report, Numerical Analysis - Part 2) von KISHIBE, Tadaharu, KAJI, Shojiro

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Study on the swirling flow field in a rotating cylinder (Numerical analysis) von KISHIBE, T, KAJI, S

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Effects of wall admittance changes on aeroelastic stability of turbomachines von Sun, Xiaofeng, Kaji, Shojiro

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Analysis of Aerodynamic Noise by Distributed Monopole Method von TAKAHASHI, Koji, KAJI, Shojiro

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Analytical Study on Plate Edge Noise : Noise Generation from Tandemly Situated Trailing and Leading Edges von Takahashi, Koji, Kaji, Shojiro

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Analysis of Unstarted Supersonic Flutter in Cascade by Semiactuator Disk Theory von Doi, Hirofumi, Kaji, Shojiro

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Effects of Wall Admittance Changes on Aeroelastic Stability of Turbomachines von Sun, Xiaofeng, Kaji, Shojiro

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Analysis of Unstarted Supersonic Flutter in Cascade by Semiactuator Disk Theory von Doi, Hirofumi, Kaji, Shojiro

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Analysis of Aerodynamic Noise by Distributed Monopole Method von Takahashi, Koji, Kaji, Shojiro

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Swirling Flow Field inside a Hollow Turbine Shaftfor an Internal Cooling Air System von Kishibe, Tadaharu, Kaji, Shojiro

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Study on the Swirling Flow Field in a Rotating Cylinder : 3rd Report, Experiment von KISHIBE, Tadaharu, KAJI, Shojiro

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Study on the Swirling Flow Field in a Rotating Cylinder. 1st Report. Numerical Analysis. Part 1 von KISHIBE, Tadaharu, KAJI, Shojiro

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Pressure field around a rectangular supersonic jet in screech von Kaji, Shojiro, Nishijima, Noriyo

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On Supersonic Jet Screech von KAJI, Shojiro

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Theoretical Study on the Unsteady Aerodynamic Characteristics of an Oscillating Cascade with Tip Clearance : In the Case of Loaded Cascade von WATANABE, Toshinori, KAJI, Shojiro

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A Study on the Convergence of Roe's Approximate Riemann Solver von MASAKI, Daisaku, KAJI, Shojiro

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Study of Transonic Cascade Airfoils by a Panel Method von SATO, Iwataro, KAJI, Shojiro

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The Effects of the Aspect Ratio of the Finite Length Slit on the Mixing in a Three Dimensional Supersonic Flow von YOKOTA, Kazuhiko, KAJI, Shojiro

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