No. |
Year |
Author |
Title |
| 619 |
1986.3 |
N. Izutsu |
Numerical and Experimental Study of Dynamics of Two-Dimensional
Body in Uniform Fow. |
| 620 |
1986.11 |
Motoki Hinada, Ryojiro Akiba, Teruo Kishi, Yasunori Matogawa and Shigeki Tsukamoto |
Destruction Test of Small Scaled Solid Propellant Motors. |
| 621 |
1987.3 |
Yu Shaohua |
Adaptive Control of Large Space Structure (LSS). |
| 622 |
1987.7 |
Y. Inatani |
On the Dynamic Behavior of Balloon during its Launch; Application
of Panel Method and Extension to Unsteady Problem. |
| 623 |
1987.10 |
Y. Inatani, K. Sato and K. Karashima |
High Speed and High Angle of Attack Wind Tunnel Test Results of the Winged Space Vehicle C-2. |
| 624 |
1987.12 |
Y. Inatani |
High Speed and High Angle of Attack Aerodynamic Characteristics of Winged Space Vehicle. |
| 625 |
1988.2 |
Y. Morita and Vinod J. Modi |
Dynamics of a Flexible Orbiting Platform with MRMS. |
| 626 |
1988.3 |
H. Kanda |
Numerical Study of the Entrance Flow and its Transition
in a Circular Pipe. |
| 627 |
1988.3 |
Y. Koshioka |
A Numerical Simulation of Two-Dimensional Transient Shear Flow. |
| 628 |
1988.3 |
H. Oguchi, M. Hatakeyama and O. Inoue |
Navier-Stokes Simulation of Shock-Tube Flows over a Wedge-Type Step by Finite Volume Method. |
| 629 |
1988.6 |
T. Shimada |
A Numerical Simulation of Flows About Two-Dimensional Bodies of Parachute-like Configuration. |
| 630 |
1988.7 |
K. Yonemoto and Yoshifumi Inatani |
Analytical Interpretation on Lateral /Directional Stability and Controllability of High Angle-of-Attack Reentry Flight. |
| 631 |
1988.7 |
T. Abe |
Transport Coefficients in Direct Simulation Monte Carlo Method for Rarefied Gas Flow. |
| 632 |
1988.7 |
Y. Nakamura and J. Chutia |
Reflection of Ion-Acoustic Waves from Bipolar Potential Structures. |
| 633 |
1988.10 |
J. Onoda, N. Watanabe, K. Ichida, Y. Hashimoto, A. Nakada
and H. Saito |
Two-Dimensionally Deployable "SHDF" Truss. |
| 634 |
1988.10 |
S. Tsukamoto |
Development of a New Redundant Flight Safety System Using
Inertial Sensors. |
| 635 |
1989.2 |
S. Tsukamoto |
On the Simulation Test for the Relative Motion of Separated
Sub-Boosters on M-3S II with Nearly Half a Model Vehicle ST-735 and their
Motion Analyses Using Inertial Sensors Output. |
| 636 |
1989.3 |
T. Abe, S. Sato, K. Nakajima, K. Toki and K. Kuriki |
Quasi-steady Operation of Repetitively-pulsed Laser Thruster. |
| 637 |
1989.9 |
S. Kawamura, J. Mizuno, J. Hirao, N. Kawashima, R. Schilling |
10m Prototype for the Laser Interferometer Gravitational Wave Antenna. |
The Institute of Space and Aeronautical Science Report
