New Results in Numerical and Experimental Fluid Mechanics VI
New Results in Numerical and Experimental Fluid Mechanics VI

New Results in Numerical and Experimental Fluid Mechanics VI


     0     
5
4
3
2
1



International Edition


About the Book

Airplane Acrodynamics.- An Airbrake Design Methodology for Steep Approaches.- High-Reynolds-Number Design of a Wing Section Including Control of Boundary Layer Properties.- Numerical Analysis of Wing Vortices.- Studies on Tailplane Stall for a Generic Transport Aircraft Wind Tunnel Model.- URANS and DES Simulation of Flow Around a Rectangular Cylinder.- Active Manipulation of a Rectangular Wing Vortex Wake with Oscillating Ailerons and Winglet-Integrated Rudders.- A New Actuator Disk Model for the TAU Code and Application to a Sailplaine with a Folding Engine.- Design of a Retrofit Winglet for a Transport Aircraft with Assessment of Cruise and Ultimate Structural Loads.- Flow Control.- Numerical Simulation of a Wing with a Gapless High-Lift System Using Circulation Control.- Shock Control Bumps on Flexible and Trimmed Transport Aircraft in Transonic Flow.- A Flat Plate Experiment for Investigations of Vortex Generator Jets at High Reynolds Number.- Experimental Simulation and Test Techniques.- Measurement of Unsteady Surface Forces by Means of Piezoelectrical Copolymer Coatings.- Studies of Reynolds Number Effects on Wing Tip Vortex Positions by Means of Laser Light Sheet (LLS) and Background Oriented Schlieren (BOS) Technique Under Cryogenic Conditions.- Project ForMEx - A New CFD Approach for Transposition of Wind Tunnel Data Towards Flight Conditions.- Pressure and Heat Flux Measurements on the Surface of a Low-Aspect-Ratio Circular Cylinder Mounted on a Ground Plate.- An Investigation into Internal and External Force Balance Configurations for Short Duration Wind Tunnels.- Numerics.- Multiple Discipline Take-Off Weight Minimization for a Supersonic Transport Aircraft.- Three-Dimensional Discontinuous Galerkin Codes to Simulate Viscous Flow by Spatial Discretization of High Order and Curved Elements on Unstructured Grids.- The Space-Time Expansion DG Method.- The Parallel Mesh Deformation of the DLR TAU-Code.- Simulation of Oscillating Airfoils and Moving Flaps Employing the DLR-TAU Unsteady Grid Adaptation.- RANS Simulations with One and Six Degrees of Freedom Rigid Body Motions.- Improvement of the Automatic Grid Adaptation for Vortex Dominated Flows Using Advanced Vortex Indicators with the DLR-Tau Code.- Adjoint Algorithms for the Optimization of 3d Turbulent Configurations.- Enhanced Runge-Kutta/Implicit Methods for Solving the Navier-Stokes Equations.- Laminar Flow Control and Transition.- Navier-Stokes High-Lift Airfoil Computations with Automatic Transition Prediction Using the DLR TAU Code.- Manipulation of Attachment Line Transition by Geometry Modification at the Slat of a Multi-element Airfoil.- Using CryoTSP as a Tool for Transition Detection and Instability Examination at High Reynolds Numbers.- Direct Numerical Simulation of a Short Laminar Separation Bubble and Early Stages of the Bursting Process.- Experimental Investigations of Controlled Transition in a Laminar Separation Bubble at an Axisymmetric Diffuser.- Development of a Sensor-Actuator-System for Active Control of Boundary Layer Instabilities in Compressible Flows.- Evaluation of Initial Amplitudes of Free-Stream Excited Tollmien-Schlichting Waves from Flight-Test Data.- The Role of Turbulent Dissipation for Flow Control of Near-Wall Turbulence.- Hypersonic Flows.- Radical Farming in Scramjets.- Aerothermodynamic Investigation of the Pre-X Configuration in HEG.- SHEFEX - A First Aerodynamic Post-flight Analysis.- Simulation of Magnetohydrodynamic Effects on an Ionised Hypersonic Flow by Using the TAU Code.- Heat Fluxes Inside a Cavity Placed at the Nose of a Projectile Measured in a Shock Tunnel at Mach 4.5.- Experimental Investigation and Numerical Simulation on a Missile Radome at Mach 6.- Turbomachines.- Control of Flow Separation in Adverse Pressure Gradients by Means of Crosswise Grooved Surfaces for Turbo Machine Applications.- Wave Drag Reduction Approach for Lattice Wings at High Speeds.- Forces and Velocity Measurements in Ship Propulsion Sy


Best Sellers



Product Details
  • ISBN-13: 9783642093876
  • Publisher: Springer-Verlag Berlin and Heidelberg GmbH & Co. KG
  • Binding: Paperback
  • Height: 234 mm
  • No of Pages: 474
  • Series Title: Notes on Numerical Fluid Mechanics and Multidisciplinary Des
  • Sub Title: Contributions to the 15th Stab/Dglr Symposium Darmstadt, Germany 2006
  • Width: 156 mm
  • ISBN-10: 3642093876
  • Publisher Date: 25 Nov 2010
  • Edition: 1st ed. Softcover of orig. ed. 2008
  • Language: English
  • Returnable: Y
  • Spine Width: 25 mm
  • Weight: 730 gr


Similar Products

Add Photo
Add Photo

Customer Reviews

REVIEWS      0     
Click Here To Be The First to Review this Product
New Results in Numerical and Experimental Fluid Mechanics VI
Springer-Verlag Berlin and Heidelberg GmbH & Co. KG -
New Results in Numerical and Experimental Fluid Mechanics VI
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.

New Results in Numerical and Experimental Fluid Mechanics VI

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!