Home Report, Institute of Space and Aeronautical Science, University of Tokyo


No.392 - No.399

No.

Year

Author

Title
392 1965.1 Keiichi Karashima Second-Order Supersonic Small Disturbance Theory.
393 1965.1 Koichi Oshima, Katsutaka Sugaya, Masao Yamamoto and Toshio Totoki Diffraction of a Plane Shock Wave Around a Corner.
394 1965.1 Hakuro Oguchi, Hiroki Honma and Katsushi Funabiki Experimental Studies in a Low Density Gun Tunnel Stream.
395 1965.2 Akira Iwama, Kiroku Yamazaki and Ken Kikuchi Theoretical Performances of Hypergolic Propellant Dimazine-Chlorine Trifluoride Systems.
396 1965.3 Jiro Horikoshi A Research on the Improvement of Flying Qualities of Piloted Airplanes. -Reduced Stiffness concept Applied to Elevator Control System-
397 1965.3 Koichi Oshima Propagation of Non-Uniform Shock Waves.
398 1965.10 Minoru Okada, Jun Tamiya and Masatoshi Ito Air Traffic Control Automation in Japan.
399 1965.12 Akira Azuma Linear Dynamic Analysis of the Spinning Axisymmetrical Rocket of Vehicle.

| No.392-399 | No.400-407 | No.408-418 | No.419-433 | No.434-442 | No.443-458 | -->

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Home Report, Institute of Space and Aeronautical Science, University of Tokyo