Report, Aeronautical Research Institute, University of Tokyo
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 No. |
Year |
Author |
Title |
| 361 | 1961.2 | Humio Naruse | Approximate Solution of the Hypersonic Laminar Boundary Layer Equations with Heat Transfer and Arbitrary Pressure Gradient and Their Applications |
| 362 | 1961.2 | Yasuhiko Aihara | Stability of the Compressible Boundary Layer along a Curved Wall under Gortler-Type Disturbances. |
| 363 | 1961.3 | Keiichi Karashima | Instability of Shock Wave on Thin Airfoil High Subsonic Flow/ |
| 364 | 1961.4 | Itiro Tani, Matsusaburo Iuchi and Hiroyuki Komoda | Experimental Investigation of Flow Separation Associated with a Step or Groove. |
| 365 | 1961.5 | Hiroshi Tsuji | Ignition and Flame Stabilization in the Laminar Boundary Layer on a Porous Flat Plate with Hot Gas Injection. |
| 366 | 1961.6 | Soji Tsuchiya | Temperature Measurement by Modified Na Line Reversal Method. |
| 367 | 1961.6 | Itiro Tani | Critical Survey of Published Theories on the Mechanism of Leading-Edge Stall. |
| 368 | 1961.10 | Keiichi Karashima | Base Pressure on Two-Dimensional Blunt-Trailing Edge Wings at Supersonic Velocities. |
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| No.330-340 | No.341-349 | No.350-360 | No.361-368 | No.369-375 | No.376-378 | --> |
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