Wavenumber-Frequency Spectra on a Launch Vehicle Model Measured via Unsteady Pressure-Sensitive Paint-Reference-Cited by-同舟云学术

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Wavenumber-Frequency Spectra on a Launch Vehicle Model Measured via Unsteady Pressure-Sensitive Paint

Published:2019-05 Issue:5 Volume:57 Page:1801-1817
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Panda J.¹,Roozeboom N. H.¹,Ross J. C.¹

Affiliation:

1. NASA Ames Research Center, Moffett Field, California 94035

Funder

NASA Engineering Safety Center

NASA Transformational Tools and Technologies

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J057449

Reference31 articles.

1. Aero-Vibro-Acoustics: Problem Statement and Methods for Simulation-based Design Solution

2. An experimental characterisation of wall pressure wavevector-frequency spectra in the presence of pressure gradients

3. A COMPARISON OF MODELS FOR THE WAVENUMBER–FREQUENCY SPECTRUM OF TURBULENT BOUNDARY LAYER PRESSURES

4. Estimation of the turbulent boundary layer pressure wavenumber-frequency spectrum using a fixed probe pair

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1. Aeroacoustic Analysis using Dynamic Mode Decomposition of Unsteady Pressure-Sensitive Paint Measurements;AIAA SCITECH 2024 Forum;2024-01-04

2. Prediction of wall-pressure fluctuations for separating/reattaching flows applied to space launchers using zonal detached eddy simulation-based convolutional neural networks;Physics of Fluids;2023-06-01

3. Joint Acceptance Attenuation Factor of Integrated Pressure with Unsteady Pressure-Sensitive Paint Measurements;AIAA SCITECH 2023 Forum;2023-01-19

4. Spectral model of wall-pressure fluctuations applied to the transonic flow around a generic space launcher;AIAA SCITECH 2023 Forum;2023-01-19

5. Determining Flow Propagation Direction from In-Flight Array Surface Pressure Fluctuation Data;AIAA Journal;2022-10

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