[HTML][HTML] Supersonic jet noise from launch vehicles: 50 years since NASA SP-8072
CP Lubert, KL Gee, S Tsutsumi - The Journal of the Acoustical Society …, 2022 - pubs.aip.org
In 1971, the US National Aeronautics and Space Administration (NASA) published a
seminal report—NASA SP-8072—which compiled the results of the early supersonic jet …
seminal report—NASA SP-8072—which compiled the results of the early supersonic jet …
An immersed boundary fluid–structure interaction method for thin, highly compliant shell structures
A parallel computational method for simulating fluid–structure interaction problems involving
large, geometrically nonlinear deformations of thin shell structures is presented and …
large, geometrically nonlinear deformations of thin shell structures is presented and …
Nearfield summary and statistical analysis of the second AIAA sonic boom prediction workshop
MA Park, M Nemec - Journal of Aircraft, 2019 - arc.aiaa.org
A summary is provided for the Second AIAA Sonic Boom Workshop held on January 8–9,
2017, in conjunction with AIAA SciTech 2017. The workshop used four models of increasing …
2017, in conjunction with AIAA SciTech 2017. The workshop used four models of increasing …
[HTML][HTML] Large-Eddy Simulation of the unsteady supersonic flow around a Mars entry capsule at different angles of attack
Time-evolving high-fidelity simulations of an entry capsule in a supersonic flight regime have
been performed at different angles of attack (0∘, 5∘, 10∘ and 15∘) in Mars' atmosphere …
been performed at different angles of attack (0∘, 5∘, 10∘ and 15∘) in Mars' atmosphere …
High-lift common research model: RANS, HRLES, and WMLES perspectives for CLmax prediction using LAVA
View Video Presentation: https://doi. org/10.2514/6.2022-1554. vid A unified assessment of
three turbulence treatments: Reynolds Averaged Navier-Stokes (RANS), Hybrid RANS/LES …
three turbulence treatments: Reynolds Averaged Navier-Stokes (RANS), Hybrid RANS/LES …
A positivity-preserving high-order weighted compact nonlinear scheme for compressible gas-liquid flows
We present a robust, highly accurate, and efficient positivity-and boundedness-preserving
diffuse interface method for the simulations of compressible gas-liquid two-phase flows with …
diffuse interface method for the simulations of compressible gas-liquid two-phase flows with …
A history of jet noise research at the National Aeronautics and Space Administration
BS Henderson, DL Huff - The Journal of the Acoustical Society of …, 2021 - pubs.aip.org
This paper reviews jet noise research conducted at the National Aeronautics and Space
Administration (NASA) from the early 1950s to the present day. Research conducted by …
Administration (NASA) from the early 1950s to the present day. Research conducted by …
Near-field plume-surface interaction and regolith erosion and dispersal during the lunar landing
A rocket plume im**ing on the lunar surface when a lunar lander approaches a landing
site can cause significant dust dispersal. This study investigated the near-field rocket plume …
site can cause significant dust dispersal. This study investigated the near-field rocket plume …
Development of immersed boundary computational aeroacoustic prediction capabilities for open-rotor noise
A sharp immersed boundary computational aeroacoustic simulation approach for open-rotor
direct noise predictions is presented. A specific feature of the finite-difference based …
direct noise predictions is presented. A specific feature of the finite-difference based …
Low-boom demonstrator near-field summary for the third AIAA sonic boom prediction workshop
MA Park, MB Carter - Journal of Aircraft, 2022 - arc.aiaa.org
A summary and statistical analysis of the near-field computational fluid dynamics (CFD)
submissions for the Third AIAA Sonic Boom Prediction Workshop is provided with a focus on …
submissions for the Third AIAA Sonic Boom Prediction Workshop is provided with a focus on …