M. Ueno

发表

MECHANICAL SIGNIFICANCE OF PROBABILITY OF FAILURE AS AN INDEX FOR PREDICTION OF SLOPE FAILURE

M. Matsuo, M. Ueno, 1981 .

Lift and Lift-Induced Drag Computation by Lamb Vector Integration

R. Tognaccini, M. Ueno, C. Marongiu, 2013 .

Investigation of Indirect Reynolds Number Effect via Computational Fluid Dynamics Simulations

Wataru Yamazaki, M. Ueno, S. Yamagishi, 2017, Journal of Aircraft.

CFD-Aided Model Deformation Corrections of NASA Research Model Wind Tunnel data

K. Yasue, M. Ueno, Seigo Koga, 2015 .

Calibration of the test section Mach number in the JAXA 2m x 2m Transonic Wind Tunnel

Masataka Kohzai, Norikazu Sudani, M. Ueno, 2008 .

Intrinsic Pair Operators and the Number-Conserved Treatment of Pairing Correlations in Nuclei

M. Ueno, Y. Miyanishi, D. Hayashi, 2001, nucl-th/0111018.

A New Description of Nuclear Rotational Motion in Terms of the Intrinsic Pair Mode

M. Ueno, Y. Miyanishi, D. Hayashi, 2001, nucl-th/0111017.

Experimental study on friction and bearing capacity of caisson type pile under considering ground reinforcement

M. Ueno, N. Nakatani, 2008 .

Lift Induced Drag Computation by Lamb Vector Integration

R. Tognaccini, M. Ueno, C. Marongiu, 2010 .

Overview of the Aero- and Aerothermodynamic Research in HOPE-X and Related Activities in Japan

Masao Shirouzu, Takeshi Ito, Shigeya Watanabe, 2004 .

Model Deformation Corrections of NASA Common Research Model Using Computational Fluid Dynamics

Makoto Ueno, Kanako Yasue, K. Yasue, 2016 .

Far-Field Drag Analysis of NASA Common Research Model Simulation

Kazuomi Yamamoto, Kentaro Tanaka, Mitsuhiro Murayama, 2011 .

Summary of JAXA Studies for the Fifth AIAA CFD Drag Prediction Workshop Using UPACS and FaSTAR

Yasushi Ito, Kazuomi Yamamoto, Mitsuhiro Murayama, 2013 .

Wall and support interference corrections of NASA common research model wind tunnel tests in JAXA

Seigo Koga, Masataka Kohzai, Makoto Ueno, 2013 .

Analysis of NASA Common Research Model Dynamic Data in JAXA Wind Tunnel Tests

Seigo Koga, Masataka Kohzai, Makoto Ueno, 2013 .

80% Scaled NASA Common Research Model Wind Tunnel Test of JAXA at Relatively Low Reynolds Number

Seigo Koga, Masataka Kohzai, Makoto Ueno, 2013 .

Refinement of Boundary-Layer Detection for Drag Decomposition of Computational Subsonic Flow Field

Yoshiaki Nakamura, M. Ueno, Yoshiaki Nakamura, 2014 .

Normalization of Wind-Tunnel Data for NASA Common Research Model

Yoshiaki Nakamura, Seigo Koga, Masataka Kohzai, 2015 .

Transonic Wind Tunnel Test of the NASA CRM: Volume 1

Seigo Koga, Masataka Kohzai, M. Ueno, 2014 .

Drag Decomposition Analysis of CFD Data of the DLR-F6 Model

Makoto Ueno, Junichi Akatsuka, Akiko Hidaka, 2008 .

Unsteady Pressure Measurement of Transonic Buffet on NASA Common Research Model

Shunsuke Koike, Atsushi Hashimoto, Makoto Ueno, 2016 .

CFD-Based Assessment of Aerodynamic Design for the “PUPA™ Heavy” eVTOL/Ground Dual-Use Cargo Pod

M. Ueno, Y. Ueno, Yuichi Ito, 2020, AIAA Scitech 2021 Forum.

Evaluation of wall-interference correction method using numerical analysis and porous wall model

Atsushi Hashimoto, Taisuke Nambu, Keiichi Murakami, 2015 .

Japan Aerospace Exploration Agency Studies for the Fifth AIAA Drag Prediction Workshop

Kazuomi Yamamoto, Kentaro Tanaka, Mitsuhiro Murayama, 2014 .

UNSTEADY AERODYNAMICS OF ROLLING THICK DELTA WING WITH HIGH ASPECT RATIO

Takashi Matsuno, Yoshiaki Nakamura, Makoto Ueno, 1998 .

Unsteady Analysis of Aerodynamic Derivatives on Standard Dynamics Model

Atsushi Hashimoto, Keiichi Murakami, Makoto Ueno, 2013 .

RELIABILITY-BASED DESIGN UNDER CONSIDERATION OF UNCERTAINTY OF EXTERNAL FORCES WITHIN LIFE SPAN OF STRUCTURE

Minoru Matsuo, Makoto Ueno, M. Matsuo, 1979 .