Advances in Simulation of Wing and Nacelle Stall - Bookswagon
Home > Technology & Engineering > Mechanical engineering & materials > Mechanical engineering > Tribology (friction & lubrication) > Advances in Simulation of Wing and Nacelle Stall
Advances in Simulation of Wing and Nacelle Stall

Advances in Simulation of Wing and Nacelle Stall


     0     
5
4
3
2
1



International Edition


About the Book

The Delay of RANS-to-LES Transition in Hybrid RANS-LES Approaches and Some Recently Proposed Remedies.- Computations of Separated Flows with a Hybrid RANS/LES Approach.- Hybrid RANS/LES Study of the Development of
an Airfoil-Generated Vortex.- Interaction of Three-Dimensional Disturbances with the Flow around a Two-Element High-Lift
Airfoil.- The Discontinuous Galerkin Method as an
Enabling Technology for DNS and LES of Industrial Aeronautical Applications.- Body Force Modelling of Internal Geometry for
Jet Noise Prediction.- Numerical Studies of Turbulent Flow Influence
on a Two-Element Airfoil.- CFD for Prediction of Flow Separation from Aircraft Tail Surfaces.- Zonal RANS-LES Computation for
Near-Stall-Airfoil Flow.- Criteria for Crosswind Variations during
Approach and Touchdown at Airports.- Development and Improvement of Two Methods of Different Complexity to Simulate
Atmospheric Boundary Layer Turbulence for Aircraft Design Studies.- Simulation of Interaction of Aircraft with Gust and Resolved
LES-Simulated Atmospheric Turbulence.- A New Method to Generate Anisotropic Synthetic Turbulence for LES.- Numerical Simulation of the Turbulent Flow Around a Wing.- Integration- and Intake-Induced Flow Distortions and their Impact on Aerodynamic Fan Performance.- Flow Investigations in a Stalling Nacelle Inlet Under Disturbed Inflow.- Realistic Inlet Distortion Patterns Interacting with a Transonic Compressor Stage.- Unsteady CFD Simulation of Transonic Axial Compressor Stages with Distorted Inflow.- Transitional Shock-Wave/Boundary-Layer Interactions in Intakes at Incidence.-Advanced Design Approach for a High-lift Wind Tunnel Model Based on Flight Test Data.- Simulation of Longitudinal Vortices on a High-LiftWing.- Impact of Different UHBR-Engine Positions on the Aerodynamics of a High-LiftWing.- Numerical Investigation of the Influence of Pressure Belts on the Stall of a Transport Aircraft in Landing Configuration.- Numerical Studies of Active Flow Control Applied at the Engine-Wing Junction.


Best Sellers



Product Details
  • ISBN-13: 9783319211268
  • Publisher: Springer
  • Publisher Imprint: Springer
  • Edition: 1st ed. 2016
  • Language: English
  • Returnable: Y
  • Spine Width: 24 mm
  • Weight: 820 gr
  • ISBN-10: 3319211269
  • Publisher Date: 21 Jul 2015
  • Binding: Hardback
  • Height: 234 mm
  • No of Pages: 413
  • Series Title: Notes on Numerical Fluid Mechanics and Multidisciplinary Des
  • Sub Title: Results of the Closing Symposium of the Dfg Research Unit for 1066, December 1-2, 2014, Braunschweig, Germany
  • Width: 156 mm


Similar Products

Add Photo
Add Photo

Customer Reviews

REVIEWS      0     
Click Here To Be The First to Review this Product
Advances in Simulation of Wing and Nacelle Stall
Springer -
Advances in Simulation of Wing and Nacelle Stall
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.

Advances in Simulation of Wing and Nacelle Stall

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

    New Arrivals



    Inspired by your browsing history


    Your review has been submitted!

    You've already reviewed this product!