Shopping Cart

No products in the cart.

ESDU 21002:2021

$89.05

Viscous Full-Potential (VFP) Method for Three Dimensional Wings and Wing-Body Combinations – Part 4: VFP Analysis Programs for Flow Breakdown and Forces and Loads

Published By Publication Date Number of Pages
ESDU 2021-05 NA
Guaranteed Safe Checkout
Category:

If you have any questions, feel free to reach out to our online customer service team by clicking on the bottom right corner. We’re here to assist you 24/7.
Email:[email protected]

The VFP wing-body method1 is ideally suited for concept and preliminary design studies as the method can rapidly produce results and does not require prolonged set up times. This means that complete polars can be produced in hours, generating a large amount of data which can be analysed as part of the decision-making process before the next variation of the design can be investigated. To help improve and reduce the analysis time a VFP analysis program has been written to read data from selected VFP output files to produce a set of files which are in a format which can be easily copied and pasted into Microsoft Office Excel spreadsheets. There are two Excel spread sheets, which have been set up to display the data in a form which will enable a quick assessment of the design, covering the operating envelope of the aircraft. One of the Excel spread sheets covers the loads and the other shock induced separation and low speed clean wing CL max.

ESDU 21002:2021
$89.05