Summary of Flow Modulation and FluidStructure Interaction Findings: Results of the Collaborative Research Center SFB 401 at the,Used

Summary of Flow Modulation and FluidStructure Interaction Findings: Results of the Collaborative Research Center SFB 401 at the,Used

In Stock
SKU: DADAX3642263720
Brand: Springer
Condition: New
Regular price$267.20
Quantity
Add to wishlist
Add to compare

Sold by Ergodebooks, an authorized reseller.

Returns accepted within 30 days | support@ergodebooks.com

Verified
Shipping Information
  • Free Standard Shipping — United States only
  • Processing Time: 1–3 business days
  • Estimated Delivery: 3–5 business days after dispatch
  • Double-boxed, fully insured & discreetly packaged
  • Tracking number sent via email once dispatched
  • Orders over $250 require signature upon delivery. Taxes calculated at checkout.
Returns & Refund

Returns accepted within 30 days of delivery.

Damaged or Defective Item

Free return shipping + replacement or full refund

Wrong Item Received

Free return shipping + replacement or full refund

Change of Mind

Return shipping at customer's expense · 25% restocking fee applies

All returns require a Return Authorization (RA) number before sending.

To initiate a return, contact us:

support@ergodebooks.com +1 (281) 738-1050
View Full Return & Refund Policy
Payment Option
Payment Methods

Help

If you have any questions, you are always welcome to contact us. We'll get back to you as soon as possible, withing 24 hours on weekdays.

Customer service

All questions about your order, return and delivery must be sent to our customer service team by e-mail at yourstore@yourdomain.com

Sale & Press

If you are interested in selling our products, need more information about our brand or wish to make a collaboration, please contact us at press@yourdomain.com

Vortex Sheets of Aircraft in Takeoff and Landing. An Adaptive Implicit Finite Volume Scheme for Compressible Turbulent Flows about Elastic Configurations. Timestep Control for Weakly Instationary Flows. Adaptive Multiscale Methods for Flow Problems: Recent Developments. Interaction of WingTip Vortices and Jets in the Extended Wake. Experimental and Numerical Investigation of Unsteady Transonic Airfoil Flow. Enabling Technologies for Robust HighPerformance Simulations in Computational Fluid Dynamics. Influencing Aircraft Wing Vortices. Development of a Modular Method for Computational Aerostructural Analysis of Aircraft. A Unified Approach to the Modeling of Airplane Wings and Numerical Grid Generation Using BSpline Representations. Parallel and Adaptive Methods for FluidStructureInteractions. Iterative Solvers for Discretized Stationary Euler Equations. Unsteady Transonic Fluid Structure Interaction at the BAC 311 High Aspect Ratio Swept Wing. Structural Idealization of Flexible Generic Wings in Computational Aeroelasticity. Aerostructural Dynamics Experiments at High Reynolds Numbers.

⚠️ WARNING (California Proposition 65):

This product may contain chemicals known to the State of California to cause cancer, birth defects, or other reproductive harm.

For more information, please visit www.P65Warnings.ca.gov.

Recently Viewed