AIAA Journal
IF
2.13
Papers
23.2k
Papers 10,000
1 page of 1,000 pages (10k results)
Newest
#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...
Source
#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...
Source
#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...
Source
#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...
Source
#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...
Source
#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...
Source
#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 ...
Source
#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...
Source
#1Pedro Gomes (Imperial College London)H-Index: 2
#2Rafael Palacios (Imperial College London)H-Index: 28
Source
#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)...
Source
12345678910
Top fields of study
This website uses cookies.
We use cookies to improve your online experience. By continuing to use our website we assume you agree to the placement of these cookies.
To learn more, you can find in our Privacy Policy.