MURAKAMI Akira

J-GLOBAL         Last updated: Feb 2, 2010 at 00:00
 
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Name
MURAKAMI Akira
Affiliation
Japan Aerospace Exploration Agency
Section
Aviation Program Group Supersonic Transport Team
Job title
Chief Manager for Planning
Degree
Doctor of Engineering(The University of Tokyo)

Research Areas

 
 

Academic & Professional Experience

 
1989
   
 
National Aerospace Laboratory, Researcher
 
1991
   
 
Technical Official, Agency of Industrial Science and
 
 
   
 
Technology
 
1995
   
 
Senior Researcher, National Aerospace Laboratory
 
1997
   
 
Deputy Director, Aeronautics and Space Development
 

Education

 
 
 - 
1989
Aerospace Engineering, Graduate School, Division of Engineering, The University of Tokyo
 
 
 - 
1984
Deparment of Aeronautics, Faculty of Engineering, The University of Tokyo
 

Misc

 
Mach 3 Wind Tunnel Test of Mixed Compression Supersonic Inlet
AIAA-92-3625 (July 1992)   
Boundary Layer Transition on Swept Cylinders at Hypersonic Speeds
AIAA Journal Vol.34 (April 1996)   
Pressure Fluctuations due to Shock-wave/Boundary-layer Interaction Induced by Swept Blunt Fin
AIAA 96-4538 (Nov. 1996)   
Design Evaluation of a Hypersonic Inlet for a SST/HST Engine by CFD and Test
ISABE 97-7030 (May 1997)   
The Aerodynamic Design and Wind Tunnel Tests of a Combined Intake for a Supersonic Transport
ISABE 97-7031 (May 1997)   

Research Grants & Projects

 
Aerodynamic Design for supersonic Air-Intake
Ordinary Research
Project Year: 1989   
Silent Supersonic Technology Demonstration Program
0130 (Japanese Only)