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Report, Aeronautical Research Institute, Tokyo Imperial University |
|
No. |
Year |
Author |
Title |
172 | 1939 | Sandi Kawada | Calculation of Induced Velocity by Helical Vortices and Its Application to Propeller Theory. |
173 | 1939 | T. Sasaki and K. Hattori | On the Effect of the Density of the Air upon the Pitot-static Tube Coefficient. |
174 | 1939 | Masaharu Goto and Hirosi Tanaka | Some Studies on Wire-Drawing. |
175 | 1939 | ØšGEīj | qóĪ·Ģ@Ėî{qąŦ\ĀŠĘ@(Flight Tests on the Range of the Koken Long-Range Monoplane.) |
176 | 1939 | ēRåOEüāVõMEŽŅūOY | ûüTmíÉÂĒÄ@(On Direction Finder.) |
177 | 1939 | Umejiro Yosida | On the Sodium Line Reversal Method of Determining the Temperature in a Gasoline Engine. |
178 | 1939 | ēRåO | PõĘ^ÉAĒÄ@(On the Simple-Chromatic Photograph.) |
179 | 1939 | Juichi Obata, Yahei Yosida and Umeziro Yosida | Measurement of Pressure-Variations in the Neigh-bourhood of the Airscrew Blade. (experiments with Actual Airscrew.) |
180 | 1939 | Susumu Tomotika and Isao Imai | On the Velocity Distribution in Turbulent Flow through a Straight Pipe of Annular Cross-section. |
181 | 1939 | Katsutada Sezawa and Ikuo Utida | On the Frequency of Flexural Vibrations of a Rotating Propeller Blade. |
182 | 1939 | Susumu Tomotika ,Ko Tamada and Yukimasa Saito | Note on the effect of Boundary Walls of a Stream upon the Circulation round a Plane Aerofoil. |
183 | 1939 | Isao Imai | On the Deformation of Free Boundary due to Line Vortices. |
184 | 1939 | ēRåOEOqņYEHÂYO | âpíĖĪięj@(Uber Radiator (I).) |
185 | 1939 | Susumu Tomotika and Hazimu Umemoto | The Forces on a Plane Aerofoil in a Wind Tunnel of the Gottingen Type, with special Reference to Approximate Formula for the Lift. |
186 | 1939 | Syuiti Kiuti | A Singular Transformation on the Surface Part of the Fe-Ni-Al System. |
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