Relevant bibliographies by topics / Jet Blast Deflector

Contents

  1. Journal articles
  2. Conference papers

Academic literature on the topic 'Jet Blast Deflector'

Author: Grafiati
Published: 6 September 2023

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the lists of relevant articles, books, theses, conference reports, and other scholarly sources on the topic 'Jet Blast Deflector.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Journal articles on the topic "Jet Blast Deflector"

1

Ma, Song, Jianguo Tan, Xiankai Li, and Jiang Hao. "The effect analysis of an engine jet on an aircraft blast deflector." Transactions of the Institute of Measurement and Control 41, no. 4 (2018): 990–1001. http://dx.doi.org/10.1177/0142331218755892.

Full text
Abstract:
This paper establishes a novel mathematical model for computing the plume flow field of a carrier-based aircraft engine. Its objective is to study the impact of jet exhaust gases with high temperature, high speed and high pressure on the jet blast deflector. The working condition of the nozzle of a fully powered on engine is first determined. The flow field of the exhaust jet is then numerically simulated at different deflection angle using the three-dimensional Reynolds averaged Navier–Stokes equations and the standard [Formula: see text]-[Formula: see text] turbulence method. Moreover, infra
APA, Harvard, Vancouver, ISO, and other styles
2

Worden, Theodore J., Chiang Shih, and Farrukh S. Alvi. "Supersonic Jet Impingement on a Model-Scale Jet Blast Deflector." AIAA Journal 55, no. 8 (2017): 2522–36. http://dx.doi.org/10.2514/1.j055664.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Miller, SAE, and Alexander N. Carr. "Theoretical investigation of alteration and radiation of large-scale structures due to jet impingement." International Journal of Aeroacoustics 18, no. 2-3 (2018): 231–57. http://dx.doi.org/10.1177/1475472x18812810.

Full text
Abstract:
Jet flows impinge on launch pad structures and aircraft carrier deck blast deflectors. Turbulent structures are deformed and acoustic radiation is reflected by the deflector. The coupling of reflected acoustic waves with the instability waves of the jet turbulence increases their amplitude and causes a feedback loop. Resultant far-field acoustic radiation is amplified. This amplification results in additional tones with significant spectral broadening occurring at frequencies corresponding to the constructive interference. We present a simple prediction methodology in the form of an acoustic a
APA, Harvard, Vancouver, ISO, and other styles
4

Natarajan, Karthikeyan, and Lakshmi Venkatakrishnan. "Flow and acoustic investigations into the impingement of single and multiple jets onto a jet blast deflector." Journal of the Acoustical Society of America 146, no. 4 (2019): 3041. http://dx.doi.org/10.1121/1.5137537.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Bendersky, Leonid Aleksandrovich, Dmitriy Aleksandrovich Lyubimov, and Aleksandra Olegovna Chestnykh. "NUMERICAL INVESTIGATION ON THE INTERACTION OF A PAIR OF HOT OFF-DESIGN SUPERSONIC JETS WITH A JET BLAST DEFLECTOR." TsAGI Science Journal 49, no. 1 (2018): 13–28. http://dx.doi.org/10.1615/tsagiscij.2018026782.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Waghmare, Utkarsh, A. S. Dhoble, Ravindra Taiwade, Jagesvar Verma, and Himanshu Vashishtha. "Prediction of heat affected zone and other mechanical properties of welded joints of HSLA A588-B of jet blast deflector." World Journal of Engineering 16, no. 4 (2019): 438–44. http://dx.doi.org/10.1108/wje-08-2018-0281.

Full text
Abstract:
Purpose The purpose of this paper is to predict and optimize the width of heat affected zone (HAZ) with better mechanical properties using suitable welding process and parameters for the fabrication of jet blast deflector (JBD) (high strength low alloy material of grade A588-B was used for fabrication) so that the JBD can sustain high exhaust parameters, because there are different welding zones formed due to the rapid cooling of weld metals. Out of the various zones of welding, HAZ remains the weakest zone in the entire weldment. Design/methodology/approach The present work describes the mode
APA, Harvard, Vancouver, ISO, and other styles
7

Benderskii, L. A., D. A. Lyubimov, A. O. Chestnykh, B. M. Shabanov, and A. A. Rubakov. "The Use of the RANS/ILES Method to Study the Influence of Coflow Wind on the Flow in a Hot, Nonisobaric, Supersonic Airdrome Jet during Its Interaction with the Jet Blast Deflector." High Temperature 56, no. 2 (2018): 247–54. http://dx.doi.org/10.1134/s0018151x18020037.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Gao, Fu-Dong, De-Xin Wang, Hai-Dong Wang, and Ming-Ming Jia. "Numerical Analysis and Verification of the Gas Jet from Aircraft Engines Impacting a Jet Blast Deflector." Chinese Journal of Mechanical Engineering 31, no. 1 (2018). http://dx.doi.org/10.1186/s10033-018-0285-7.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Erwin, James P., Neeraj Sinha, and Gregory P. Rodebaugh. "Large Eddy Simulations of Supersonic Impinging Jets." Journal of Engineering for Gas Turbines and Power 134, no. 12 (2012). http://dx.doi.org/10.1115/1.4007338.

Full text
Abstract:
Supersonic impinging jet flow fields contain self-sustaining acoustic feedback features that create high levels of tonal noise. These types of flow fields are typically found with short takeoff and landing military aircraft as well as jet blast deflector operations on aircraft carrier decks. The United States Navy has a goal to reduce the noise generated by these impinging jet configurations and is investing in computational aeroacoustics to aid in the development of noise reduction concepts. In this paper, implicit large eddy simulation (LES) of impinging jet flow fields are coupled with a fa
APA, Harvard, Vancouver, ISO, and other styles

Conference papers on the topic "Jet Blast Deflector"

1

Jaiswal, Abhijeet, Ashwin S. Dhoble, and D. J. Tidke. "High Compressible Flow Through Jet Blast Deflector." In ASME 2017 Gas Turbine India Conference. American Society of Mechanical Engineers, 2017. http://dx.doi.org/10.1115/gtindia2017-4699.

Full text
Abstract:
Jet blast impact on aerofoil blade of the deflector is studied which redirects the high energy exhaust of jet engine during the ground testing. The geometric model of aerofoils is designed with structured mesh around the aerofoil in rectangular domain generated in ICEM 16 software. The jet blast impact on aerofoil blade of the deflector is numerically simulated with SST k-ω model based on CFD theory. The fluid flow is high-speed compressible flow and flowing fluid air is considered as an ideal gas and also Sutherland’s law viscosity is applied to account for the dependence of molecular viscosi
APA, Harvard, Vancouver, ISO, and other styles
2

Worden, Theodore J., Chiang Shih, and Farrukh S. Alvi. "Supersonic Jet Impingement on a Model-scale Jet Blast Deflector." In 54th AIAA Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-1015.

Full text
APA, Harvard, Vancouver, ISO, and other styles
3

Alostaz, Yousef, Mark Fantozzi, and Peter Feenstra. "Innovative Jet Blast Deflector System: Analysis and Design." In Structures Congress 2015. American Society of Civil Engineers, 2015. http://dx.doi.org/10.1061/9780784479117.185.

Full text
APA, Harvard, Vancouver, ISO, and other styles
4

Tangen, Steven. "Investigating Separated Shear Layers for Passive Jet Blast Deflector Cooling." In 44th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/6.2006-144.

Full text
APA, Harvard, Vancouver, ISO, and other styles
5

Erwin, James, Neeraj Sinha, and Gregory Rodebaugh. "Noise predictions of a hot twin-jet impinging on a jet blast deflector." In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-324.

Full text
APA, Harvard, Vancouver, ISO, and other styles
6

Pilon, Anthony R. "Land- and Aircraft Carrier-Based F-35C Jet Blast Deflector Noise Testing." In 22nd AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics, 2016. http://dx.doi.org/10.2514/6.2016-2730.

Full text
APA, Harvard, Vancouver, ISO, and other styles
7

Korotaeva, T. A., and A. O. Turchinovich. "Numerical simulation of interaction between chemically active exhaust and a jet blast deflector." In PROCEEDINGS OF THE XXV CONFERENCE ON HIGH-ENERGY PROCESSES IN CONDENSED MATTER (HEPCM 2017): Dedicated to the 60th anniversary of the Khristianovich Institute of Theoretical and Applied Mechanics SB RAS. Author(s), 2017. http://dx.doi.org/10.1063/1.5007608.

Full text
APA, Harvard, Vancouver, ISO, and other styles
8

Liu, Junhui, Kailas Kailasanath, Nick Heeb, David Munday, and Ephraim Gutmark. "Impact of Deck and Jet Blast Deflector on the Flow and Acoustic Properties of Imperfectly Expanded Supersonic Jets." In 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. American Institute of Aeronautics and Astronautics, 2013. http://dx.doi.org/10.2514/6.2013-323.

Full text
APA, Harvard, Vancouver, ISO, and other styles
9

Erwin, James P., Neeraj Sinha, and Gregory P. Rodebaugh. "Large Eddy Simulations of Supersonic Impinging Jets." In ASME Turbo Expo 2012: Turbine Technical Conference and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/gt2012-70140.

Full text
Abstract:
Supersonic impinging jet flowfields contain self-sustaining acoustic feedback features that create high levels of discrete frequency tonal noise. These types of flowfields are typically found with short takeoff and landing military aircraft as well as jet blast deflector operations on aircraft carrier decks. The US Navy has a goal to reduce the noise generated by these impinging jet configurations and is investing in computational aeroacoustics to aid in the development of noise reduction concepts. In this paper, implicit Large Eddy Simulation (LES) of impinging jet flow-fields are coupled wit
APA, Harvard, Vancouver, ISO, and other styles
We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!

To the bibliography