Article
Engineering, Aerospace
Matthew W. Tufts, Matthew P. Borg, Nicholas J. Bisek, Roger L. Kimmel
Summary: High-fidelity, time-accurate solutions of the flowfield around the HIFiRE-5 wind-tunnel geometry including postshock perturbations were obtained using the Overflow computational-fluid-dynamics solver. The time-averaged results show that the method reproduces the heat-flux contours measured experimentally via thermal imaging for both quiet and noisy facilities. This method has the potential to accurately extrapolate wind-tunnel tests between facilities and potentially to flight, and can also be used as a transition prediction method for flow conditions that cannot be accessed in existing ground facilities.
Article
Engineering, Aerospace
Yatian Zhao, Zhiyuan Shao, Hongkang Liu
Summary: This study investigates the influence of aerodisk on hypersonic boundary layer transition and heat flux distribution. The results show that aerodisk can reduce the maximum wall heat flux and surface pressure, and alter the location and shape of the transition region. Additionally, the angle of attack also affects the position and form of the transition.
Article
Mechanics
V. Borodulin, A. Ivanov, Y. S. Kachanov, A. P. Roschektayev
Summary: The study focuses on experimental investigation of distributed receptivity of a laminar swept-wing boundary layer to unsteady freestream vortices. It is found that unsteady streamwise vortices efficiently excite non-stationary cross-flow instability modes without the need for surface non-uniformities. The experimental approach allows detailed quantitative investigation of the mechanism of distributed excitation of unsteady boundary-layer disturbances.
JOURNAL OF FLUID MECHANICS
(2021)
Article
Mechanics
Yufeng Han, Jingtian Zhou, Wei Cao
Summary: This study investigates the calculation of the entropy-swallowing point location and its dependence on the Mach number and Reynolds number. The results show that the location of the entropy-swallowing point is more strongly influenced by the Reynolds number, while an increase in the Mach number decreases its impact.
Article
Engineering, Multidisciplinary
Kenny Chowdhary, Chi Hoang, Kookjin Lee, Jaideep Ray, V. G. Weirs, Brian Carnes
Summary: This paper explores the effectiveness of combining machine-learning methods with projection-based model reduction techniques to create data-driven surrogate models of computationally expensive, high-fidelity physics models. The method is demonstrated on modeling heat flux and pressure in a turbulent flow and used for Bayesian estimation of parameters in a turbulence model for a high-fidelity flow simulator.
COMPUTER METHODS IN APPLIED MECHANICS AND ENGINEERING
(2022)
Article
Mechanics
Meikuan Liu, Guilai Han, Zongxian Li, Zonglin Jiang
Summary: This study investigates the hypersonic boundary-layer transition on a large-scale cone in a hypersonic flight duplicate shock tunnel. The transition Reynolds number shows a trend of first increasing and then decreasing with the increase in the bluntness Reynolds number, indicating a transition reversal phenomenon.
Article
Mechanics
Yanhua Zhu, Xinliang Li, Tongbiao Guo, Hongwei Liu, Fulin Tong
Summary: This study investigates the bluntness effect on hypersonic boundary-layer transition over a slender cone with zero angle of attack through direct numerical simulation. The results show that the transition position and region are influenced by the nose radius. While the flow transition and entropy swallowing happen almost simultaneously in the case with a 1mm nose radius, they occur earlier in the other cases. Frequency spectrum analysis reveals the presence of high frequency and extremely low frequency characteristic frequencies in all cases, with the 1mm case exhibiting significantly higher high frequency.
Article
Engineering, Aerospace
Yuanqiang Liu, Yan Liu, Zubi Ji, Yutian Wang, Jiakuan Xu
Summary: This paper investigates the suction effects and mechanism of suction control in transonic swept wing boundary layers through experiments and theoretical analysis. The delay of boundary layer transition caused by suction near the leading-edge region is validated, and the effects of curvature on stationary crossflow vortices are analyzed.
Article
Mechanics
Santhosh B. Mamidala, Andre Weingartner, Jens H. M. Fransson
Summary: To date, there have been very few comparisons between experiments and direct numerical simulations (DNS) on free-stream turbulence (FST) induced boundary layer transition. This is mainly due to the difficulty in carrying out such comparisons because of the large energy gradients and sensitivity to surrounding conditions in transition scenarios. This study presents a detailed comparison between new experiments and available DNS data of a complex FST transition scenario in a flat plate boundary layer. The leading edge pressure gradient distribution and the full energy spectrum at the leading edge are identified as the two most important parameters for a satisfying comparison. The study also defines a measure of FST boundary layer penetration depth using DNS, suggesting that the depth grows with downstream distance and stays around 20% of the boundary layer thickness down to transition onset.
JOURNAL OF FLUID MECHANICS
(2022)
Article
Mechanics
Alberto F. Rius-Vidales, M. Kotsonis
Summary: The study found that a forward-facing step has an impact on the development of stationary crossflow instability, causing abrupt changes in vortex trajectories and amplification effects. Different step heights affect the stability of the primary stationary mode and its harmonics to varying degrees. In the case of shorter step heights, velocity fluctuations eventually decrease below the level of the configuration without a step.
JOURNAL OF FLUID MECHANICS
(2021)
Article
Mechanics
Y. X. Wang, K. -S. Choi, M. Gaster, C. Atkin, V. Borodulin, Y. Kachanov
Summary: The experimental investigation in a low-turbulence wind tunnel revealed that artificially initiated turbulent spots in a laminar boundary layer over a flat plate quickly developed into hairpin-like structures, increasing in width, length and height downstream. Only disturbances greater than a threshold value evolved into turbulent spots, while others decayed. The rate of development was also influenced by the duration of initial disturbances. Additionally, the behavior of turbulence generation within a turbulent spot was found to be similar to burst events in a turbulent boundary layer.
JOURNAL OF FLUID MECHANICS
(2021)
Article
Mechanics
Sumit Tambe, Ferry Schrijer, Leo Veldhuis, Arvind Gangoli Rao
Summary: This research investigates the behavior of an unstable boundary-layer on rotating cones in high-speed flow conditions. Using infrared thermography, the instability-induced flow structures are detected, and spiral modes similar to those observed in low-speed conditions are observed.
Article
Mechanics
G. Zoppini, T. Michelis, D. Ragni, M. Kotsonis
Summary: This study experimentally characterizes the flow field near periodically spaced discrete roughness elements (DRE) in a swept wing boundary layer for the first time. Time-averaged velocity fields are obtained using high-resolution dual-pulse tomographic particle tracking velocimetry. Analysis reveals that the near-element flow region is dominated by high and low-speed streaks. The boundary layer spectral content and the evolution of disturbance energy are examined using spatial fast Fourier transform (FFT) analysis of the spanwise velocity signal. The results show significant transient growth and decay processes in both the chordwise disturbance evolution and the near-wake region after each DRE. The findings demonstrate the importance of transient disturbances and their interaction with DRE characteristics in boundary layer transition and flow tripping processes.
JOURNAL OF FLUID MECHANICS
(2023)
Article
Mechanics
Xudong Tian, Chihyung Wen
Summary: Stability analyses based on perturbation rates were used to study the growth mechanisms of second-mode instability in hypersonic boundary layers. The results revealed the interactions of streamwise velocity, wall-normal velocity, and fluctuating internal energy, with wall-normal velocity perturbation playing a key role in the growth of second-mode instability, dependent on the relative phase with the total time rate of change of fluctuating internal energy near the critical layer.
JOURNAL OF FLUID MECHANICS
(2021)
Article
Mechanics
V. Borodulin, A. Ivanov, Y. S. Kachanov, A. P. Roschektayev
Summary: The study found that unsteady streamwise vortices can efficiently excite cross-flow instability modes without the need for any surface non-uniformities. The experimental approach allows for a detailed quantitative investigation of the mechanism of distributed excitation of unsteady boundary-layer disturbances due to scattering of freestream vortices on natural base-flow non-uniformity.
JOURNAL OF FLUID MECHANICS
(2021)
Article
Engineering, Aerospace
Matthew T. Lakebrink, Kevin G. Bowcutt, Troy Winfree, Christopher C. Huffman, Thomas J. Juliano
JOURNAL OF SPACECRAFT AND ROCKETS
(2018)
Article
Engineering, Aerospace
Joseph S. Jewell, Roger L. Kimmel, David W. Adamczak, Jonathan Poggie, Kevin M. Porter, Thomas J. Juliano
JOURNAL OF SPACECRAFT AND ROCKETS
(2018)
Article
Engineering, Aerospace
Thomas J. Juliano, Laura A. Paquin, Matthew P. Borg
Article
Engineering, Mechanical
Carson L. Running, Hirotaka Sakaue, Thomas J. Juliano
EXPERIMENTS IN FLUIDS
(2019)
Article
Engineering, Aerospace
Thomas J. Juliano, Joseph S. Jewell, Roger L. Kimmel
JOURNAL OF SPACECRAFT AND ROCKETS
(2019)
Article
Engineering, Aerospace
Thomas J. Juliano, Jonathan Poggie, Kevin M. Porter, Roger L. Kimmel, Joseph S. Jewell, David W. Adamczak
JOURNAL OF SPACECRAFT AND ROCKETS
(2018)
Article
Engineering, Aerospace
Roger L. Kimmel, David W. Adamczak, Matthew P. Borg, Joseph S. Jewell, Thomas J. Juliano, Scott A. Stanfield, Karen T. Berger
JOURNAL OF SPACECRAFT AND ROCKETS
(2019)
Article
Engineering, Aerospace
Brandon C. Chynoweth, Steven P. Schneider, Christoph Hader, Hermann Fasel, Armani Batista, Joseph Kuehl, Thomas J. Juliano, Bradley M. Wheaton
JOURNAL OF SPACECRAFT AND ROCKETS
(2019)
Article
Mechanics
Harrison B. Yates, Matthew W. Tufts, Thomas J. Juliano
JOURNAL OF FLUID MECHANICS
(2020)
Article
Thermodynamics
Carson L. Running, Thomas J. Juliano, Joseph S. Jewell, Matthew P. Borg, Roger L. Kimmel
EXPERIMENTAL THERMAL AND FLUID SCIENCE
(2019)
Correction
Engineering, Aerospace
Carson L. Running, Thomas J. Juliano, Matthew P. Borg, Roger L. Kimmel
Article
Engineering, Aerospace
Andrew N. N. Bustard, Thomas J. J. Juliano, Harrison B. B. Yates, Mark Noftz, Joseph Jewell
Article
Engineering, Aerospace
Mark E. Noftz, Andrew J. Shuck, Joseph S. Jewell, Jonathan Poggie, Andrew N. Bustard, Thomas J. Juliano, Nicholas J. Bisek
Summary: This paper presents the design of an inward-turning high-speed three-dimensional streamline-traced intake using osculating axisymmetric theory. The design criteria includes a stitched Busemann diffuser and internal conical flow-A solution for efficient compression, high flow uniformity, and straight leading-edge shocks of equal strength. A novel method for constructing the inlet cowl is also introduced. The validation of the design method is done through computational fluid dynamic results of the two-dimensional parent flowfields and the full three-dimensional design.
JOURNAL OF PROPULSION AND POWER
(2023)
Article
Engineering, Aerospace
Oliver D. Wong, A. Neal Watkins, Kyle Z. Goodman, Jim Crafton, Alan Forlines, Larry Goss, James W. Gregory, Thomas J. Juliano
JOURNAL OF THE AMERICAN HELICOPTER SOCIETY
(2018)
Article
Engineering, Aerospace
Stanislav Gordeyev, Thomas J. Juliano