Buy Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications
Book 1
Book 2
Book 3
Book 1
Book 2
Book 3
Book 1
Book 2
Book 3
Book 1
Book 2
Book 3
Home > Science, Technology & Agriculture > Mechanical engineering and materials > Materials science > Engineering: Mechanics of fluids > Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications: (201 Notes on Numerical Fluid Mechanics and Multidisciplinary Design)
36%
Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications: (201 Notes on Numerical Fluid Mechanics and Multidisciplinary Design)

Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications: (201 Notes on Numerical Fluid Mechanics and Multidisciplinary Design)


     0     
5
4
3
2
1



Available


X
About the Book

This open-access book reports on both experimental and numerical findings from the H2020-funded project TEAMAero (Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications). It covers novel contributions on improving the fundamental understanding of the physics of shock wave boundary layer interaction, developments in flow control for mitigation of shock effects, and advanced numerical methods for predicting those effects. All in all, this book offers a timely snapshot of research and developments in numerical methods for flow analysis and control, with a special emphasis on high-speed flows. It offers extensive information to both researchers and professionals.

Table of Contents:
Part1.Introduction.- Part2.Numerical and experimental methods development.- 1."From high-fidelity high-order to reduced-order modeling for unsteady shock wave/boundary layer interactions ".- 2.Numerical tools for high-fidelity simulation of sblis.- 3."Development of a PVDF Piezo-Film Sensor for Unsteady Wall-Pressure Measurements in sblis".- Part3.Transitional/turbulent SBLI and flow control.- 4.Non-linearities in the low-frequency dynamics of transitional SBLI.- 5.The length and time scales of transitional sblis.- 6."Parameter Influence on Porous Bleed Performance for Shock-Wave/Boundary-Layer Interaction Control".- 7.Unsteady three-dimensional oblique shock wave boundary-layer interactions.- 8.Oblique-shock wave boundary layer interactions control: shock control bumps.- Part4.Airfoil/wing configuration.- 9.Numerical Study of Unsteady Shock/Boundary Layer Interaction.- 10.Numerical study and physical analysis of the transonic interaction and its modification through morphing around supercritical wings at high Reynolds number.- Part5.Transonic compressor.- 11.Numerical investigations of transitional SBLI on a highly loaded-transonic compressor.- 12.Reynolds number effects on shock wave boundary layer interaction in highly loaded compressor stator.- 13."Experimental and Numerical Investigations of SBLI and Flow Control on a Transonic Compressor Cascade ".- 14.Surface roughness effect on SBLI on compressor rotor profile.- 15."Shock Oscillation Mechanisms of Highly Separated Transitional Shock-Wave/Boundary-Layer Interactions".

About the Author :
Pawel Flaszynski studied mechanical engineering and obtained a Ph.D. in turbomachinery flows and inverse design from Gdansk University of Technology (Poland) in 2002. He then continued his research in the field of aerodynamics and numerical methods, focusing on flow control (streamwise vortex generators) in subsonic and transonic flows, as well as shock-wave/boundary-layer interactions. In 2018, he was awarded a prize for his research on the development of flow control methods in aeronautics by the Ministry of Science and Higher Education (Poland). Since 2014, he has been a professor at the Institute of Fluid Flow Machinery (Polish Academy of Sciences) and the head of the aerodynamics department. He has collaborated on, and coordinated, European projects related to shock-wave/boundary-layer interactions and flow control in compressors, gas turbines, and aircraft wings. He is a member of the European Turbomachinery Society (EUROTURBO) and a representative in the International Society for Airbreathing Engines (ISABE). Holger Babinsky studied aerospace engineering at Stuttgart University in Germany. He obtained a Ph.D. in hypersonic aerodynamics from Cranfield University (UK) in 1994. After 18 months as a research associate at the Shock Wave Research Center of Tohoku University in Sendai, Japan, he returned to the UK to take up a position in the Department of Engineering of the University of Cambridge. He is now the head of fluid mechanics, energy, and turbomachinery as well as a fellow of Magdalene College. His main areas of research are in the field of experimental aerodynamics and associated measurement techniques. Apart from shock-wave/boundary-layer interactions which he has studied for more than 30 years, his current research includes unsteady aerodynamics, road vehicle aerodynamics, and flow control for aircraft wings and engine inlets. He is a fellow of the Royal Academy of Engineering, the Royal Aeronautical Society, and the American Institute of Aeronautics and Astronautics. Piotr Doerffer is a professor at the Institute of Fluid Flow Machinery (a member of the Polish Academy of Sciences, IMP PAN) in Gdansk, Poland. He is involved in both experimental and numerical analyses of transonic flows with shock waves in nozzles and turbine or compressor cascades. His extensive international cooperation stems from long-term research internships at the engineering department of Cambridge University, the mechanical faculty of Karlsruhe University, and the fluid dynamicsdepartment of DLR in Göttingen. The main focus of his work has been flow control aimed at reducing shock-wave-induced separation. He has been actively involved in European collaborative research projects, including EUROSHOCK, AITEB, TLC, ERICKA, FACTOR E-BREAK, as well as coordinating projects like UFAST and TFAST. He has also coordinated Marie Curie projects. Throughout his research career at IMP PAN, he has progressed from an assistant position to the deputy director of the institute.


Best Sellers


Product Details
  • ISBN-13: 9783031866043
  • Publisher: Springer International Publishing AG
  • Publisher Imprint: Springer International Publishing AG
  • Height: 235 mm
  • No of Pages: 380
  • Series Title: 201 Notes on Numerical Fluid Mechanics and Multidisciplinary Design
  • ISBN-10: 3031866045
  • Publisher Date: 03 Jul 2025
  • Binding: Hardback
  • Language: English
  • Returnable: N
  • Width: 155 mm


Similar Products

Add Photo
Add Photo

Customer Reviews

REVIEWS      0     
Click Here To Be The First to Review this Product
Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications: (201 Notes on Numerical Fluid Mechanics and Multidisciplinary Design)
Springer International Publishing AG -
Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications: (201 Notes on Numerical Fluid Mechanics and Multidisciplinary Design)
Writing guidlines
We want to publish your review, so please:
  • keep your review on the product. Review's that defame author's character will be rejected.
  • Keep your review focused on the product.
  • Avoid writing about customer service. contact us instead if you have issue requiring immediate attention.
  • Refrain from mentioning competitors or the specific price you paid for the product.
  • Do not include any personally identifiable information, such as full names.

Towards Effective Flow Control and Mitigation of Shock Effects in Aeronautical Applications: (201 Notes on Numerical Fluid Mechanics and Multidisciplinary Design)

Required fields are marked with *

Review Title*
Review
    Add Photo Add up to 6 photos
    Would you recommend this product to a friend?
    Tag this Book Read more
    Does your review contain spoilers?
    What type of reader best describes you?
    I agree to the terms & conditions
    You may receive emails regarding this submission. Any emails will include the ability to opt-out of future communications.

    CUSTOMER RATINGS AND REVIEWS AND QUESTIONS AND ANSWERS TERMS OF USE

    These Terms of Use govern your conduct associated with the Customer Ratings and Reviews and/or Questions and Answers service offered by Bookswagon (the "CRR Service").


    By submitting any content to Bookswagon, you guarantee that:
    • You are the sole author and owner of the intellectual property rights in the content;
    • All "moral rights" that you may have in such content have been voluntarily waived by you;
    • All content that you post is accurate;
    • You are at least 13 years old;
    • Use of the content you supply does not violate these Terms of Use and will not cause injury to any person or entity.
    You further agree that you may not submit any content:
    • That is known by you to be false, inaccurate or misleading;
    • That infringes any third party's copyright, patent, trademark, trade secret or other proprietary rights or rights of publicity or privacy;
    • That violates any law, statute, ordinance or regulation (including, but not limited to, those governing, consumer protection, unfair competition, anti-discrimination or false advertising);
    • That is, or may reasonably be considered to be, defamatory, libelous, hateful, racially or religiously biased or offensive, unlawfully threatening or unlawfully harassing to any individual, partnership or corporation;
    • For which you were compensated or granted any consideration by any unapproved third party;
    • That includes any information that references other websites, addresses, email addresses, contact information or phone numbers;
    • That contains any computer viruses, worms or other potentially damaging computer programs or files.
    You agree to indemnify and hold Bookswagon (and its officers, directors, agents, subsidiaries, joint ventures, employees and third-party service providers, including but not limited to Bazaarvoice, Inc.), harmless from all claims, demands, and damages (actual and consequential) of every kind and nature, known and unknown including reasonable attorneys' fees, arising out of a breach of your representations and warranties set forth above, or your violation of any law or the rights of a third party.


    For any content that you submit, you grant Bookswagon a perpetual, irrevocable, royalty-free, transferable right and license to use, copy, modify, delete in its entirety, adapt, publish, translate, create derivative works from and/or sell, transfer, and/or distribute such content and/or incorporate such content into any form, medium or technology throughout the world without compensation to you. Additionally,  Bookswagon may transfer or share any personal information that you submit with its third-party service providers, including but not limited to Bazaarvoice, Inc. in accordance with  Privacy Policy


    All content that you submit may be used at Bookswagon's sole discretion. Bookswagon reserves the right to change, condense, withhold publication, remove or delete any content on Bookswagon's website that Bookswagon deems, in its sole discretion, to violate the content guidelines or any other provision of these Terms of Use.  Bookswagon does not guarantee that you will have any recourse through Bookswagon to edit or delete any content you have submitted. Ratings and written comments are generally posted within two to four business days. However, Bookswagon reserves the right to remove or to refuse to post any submission to the extent authorized by law. You acknowledge that you, not Bookswagon, are responsible for the contents of your submission. None of the content that you submit shall be subject to any obligation of confidence on the part of Bookswagon, its agents, subsidiaries, affiliates, partners or third party service providers (including but not limited to Bazaarvoice, Inc.)and their respective directors, officers and employees.

    Accept

    Fresh on the Shelf


    Inspired by your browsing history


    Your review has been submitted!

    You've already reviewed this product!