Report, Institute of Space and Aeronautical Science, University of Tokyo
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Report, Institute of Space and Aeronautical Science, University of Tokyo |
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 No. |
Year |
Author |
Title |
| 521 | 1975.1 | Megumi Sunakawa and Nori Kumai | Dynamic Behavior of Viscoelastic Shallow Spherical Shells. |
| 522 | 1975.1 | Hidefumi Kobatake | Detection of Echo by Linear Prediction. |
| 523 | 1975.3 | Kazuo Tanizawa and Koryo Miura | Stress Analysis of a Concave Polyhedral Shell. |
| 524 | 1975.3 | Setsuo Ohsuga | A New Inference Rule Based on an Information Structure. |
| 525 | 1975.5 | Koh-ichiro Oyama | Characteristic of the Contaminated Langmuir Probe and Countermoves for its Application to the Space Observations. |
| 526 | 1975.5 | Kazuo Masato | A Computer Program for Quantitative Analysis with Electron Probe X-ray Microanalyser. |
| 527 | 1975.5 | Kuninori Uesugi | A Graphical Solution of Optimum Time-Fixed Two-Impulse Rendezvous Problem. |
| 528 | 1975.6 | Ryuma Kawamura and Wataru Masuda | A Numerical Study on the Effects of Viscosity on the Performance of CO2 Gasdynamic Laser. |
| 529 | 1975.6 | Akira Kobayashi and Nobuo Ohtani | Experimental Study on Preceding Viscoelastic Strain Disturbances - An Inverse Problem in Dynamic Fracture - |
| 530 | 1975.6 | Osamu Ashihara | The Electron Energy Loss Rates by Polar Molecules. |
| 531 | 1975.9 | Fumio Kikuchi | Approximation in Finite Element Models. I. General Theory for Linear Problems. |
| 532 | 1975.9 | Atsushi Okajima, Hiroyuki Takata and Tsuyoshi Asanuma | Viscous Flow Around a Rotationally Oscillating Circular Cylinder. |
| 533 | 1975.10 | Atsushi Okajima, Hiroyuki Takata and Tsuyoshi Asanuma | Viscous Flow Around a Transversally Oscillating Elliptic Cylinder. |
| 534 | 1975.11 | Shin-ichi Nakao | Supersonic Flow past Conical Bodies at Large Angles of Attack. |
| 535 | 1975.11 | Wen-Jei Yang | Theory on Vaporization and Combustion of Liquid Drops of Pure Substances and Binary Mixtures on Heated Surfaces. |
| 536 | 1975.12 | Akira Azuma | Fundamental Formulation of Airship Performance and Flight Dynamics. |
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