AIAA Journal
Papers 10,000
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#1Gaetano M. D. Currao (NCKU: National Cheng Kung University)H-Index: 5
#2Wen Lih Chen (NCKU: National Cheng Kung University)H-Index: 19
Estimating heat-flux peak location and magnitude is important to efficiently design thermal protection systems of hypersonic vehicles, which are characterized by strict low-weight requirements. Thi...
#1A.V. Nenarokomov (Moscow Aviation Institute)H-Index: 9
#2Evgeniy V. Chebakov (Moscow Aviation Institute)
Last. D. M. Titov (Moscow Aviation Institute)H-Index: 4
view all 7 authors...
A reliable control of current orientation of a spacecraft is a critical task in aerospace engineering, as the loss of the spacecraft’s attitude can endanger the whole mission. This makes it importa...
#1Adrián Lozano-Durán (MIT: Massachusetts Institute of Technology)H-Index: 21
#2Sanjeeb Bose (Stanford University)H-Index: 14
Last. Parviz Moin (Stanford University)H-Index: 120
view all 3 authors...
We investigate the error scaling and computational cost of wall-modeled large-eddy simulation (WMLES) for external aerodynamic applications. The NASA Juncture Flow is used as representative of an a...
#1Ji Zhang (HIT: Harbin Institute of Technology)H-Index: 2
#2Wuxia Miao (HIT: Harbin Institute of Technology)
Last. Changguo Wang (HIT: Harbin Institute of Technology)H-Index: 15
view all 4 authors...
#1Sunyoung Lee (NMSU: New Mexico State University)H-Index: 2
#2Andreas Gross (NMSU: New Mexico State University)H-Index: 17
Implicit large-eddy simulations of reflecting shock-wave turbulent boundary-layer interactions at a freestream Mach number of 2.05 were carried out for sweep angles of 0, 20, and 40 deg. The simula...
#1Senri Miura (Keio: Keio University)
#2Masahiro Ohashi (Keio: Keio University)H-Index: 2
Last. Naoko Tokugawa (JAXA: Japan Aerospace Exploration Agency)H-Index: 9
view all 4 authors...
Drag reduction effect by uniform blowing (UB) on the pressure surface of an airfoil is investigated through wind-tunnel experiments. The experiments are conducted using a Clark-Y airfoil model. The...
#1You Wu (Beihang University)H-Index: 1
#2Yuting Dai (Beihang University)H-Index: 1
Last. Guangjing Huang (Beihang University)H-Index: 1
view all 5 authors...
This paper investigates suppressing the pitching oscillation of a NACA 0012 airfoil at a Reynolds number of 1.35×105 by using phase-shifted trailing-edge morphing. The latter considering geometric ...
#1Shaochong Yang (Hebei University)
#2Yuan Yao (Hebei University)
Last. Qing-Sheng Yang (Beijing University of Technology)H-Index: 14
view all 6 authors...
The geometrically nonlinear random vibration response of stiffened laminated plates under acoustic excitation is carried out by using the equivalent linearization (EL) technique combined with the r...
#1Pedro Gomes (Imperial College London)H-Index: 2
#2Rafael Palacios (Imperial College London)H-Index: 28
#1Vasily Gryazev (QMUL: Queen Mary University of London)H-Index: 3
#2Annabel P. Markesteijn (QMUL: Queen Mary University of London)
Last. Sergey A. Karabasov (QMUL: Queen Mary University of London)H-Index: 18
view all 3 authors...
A generalized acoustic analogy model is implemented for the hot and cold static high-speed jet cases corresponding to conditions of the Strategic Investment in Low-carbon Engine Technology (SILOET)...
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