TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

Published by THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES

738 registered articles
(updated on July 16, 2018)

Online ISSN : 2189-4205
Print ISSN : 0549-3811

0.541
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JOURNALS PEER REVIEWED PARTIALLY RESTRICTED ACCESS

2018 Volume 61 Issue 4

Effects on the Positioning Accuracy of a GPS Receiver with Array Antenna and Time Delay Compensation for Precise Anti-Jamming Kihoon LEE, Junpyo PARK, Jiyun LEE
Numerical Analysis of a Miniature Microwave-discharge Ion Thruster Using Water as the Propellant Kengo NAKAMURA, Yuichi NAKAGAWA, Hiroyuki KOIZUMI, Yoshinori TAKAO
Shape-Based, Low-Thrust Trajectory Design in Alternating Rotational Coordinate System Jun MATSUMOTO, Junichiro KAWAGUCHI
Experimental Study on Quantitative Radiation Properties of Laminar Oxygen-enriched Inverse Diffusion Flames in Gas Turbines Qitai ERI, Baolu WANG, Ting LI

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Most viewed articles Jun.2018

1

Fundamental Combustion Characteristics of Ethanol/Liquid Oxygen Rocket Engine Combustor with Planar Pintle-type Injector

Released: January 06, 2015 | Volume 58 Issue 1 Pages 15-22

Kazuki SAKAKI, Minho CHOI, Shinji NAKAYA, Mitsuhiro TSUE, Tetsuo HIRAIWA
2

Aerodynamic Analysis of the Ducted Fan for a VTOL UAV in Crosswinds

Released: March 04, 2016 | Volume 59 Issue 2 Pages 47-55

Minhyoung RYU, Leesang CHO, Jinsoo CHO
3

Comprehensive Design Method for LOX/Liquid-Methane Regenerative Cooling Combustor with Coaxial Injector

Released: November 02, 2009 | Volume 52 Issue 177 Pages 180-187

Nobuyuki YATSUYANAGI
4

Aerodynamic Characteristic Analysis of Multi-Rotors Using a Modified Free-Wake Method

Released: November 02, 2009 | Volume 52 Issue 177 Pages 168-179

Jaewon LEE, Kwanjung YEE, Sejong OH
5

Investigations on Missile Configuration Aerodynamic Characteristics for Design Optimization

Released: June 26, 2014 | Volume 57 Issue 4 Pages 210-218

Nhu-Van NGUYEN, Maxim TYAN, Jae-Woo LEE, Yung-Hwan BYUN

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