Advances in simulation of wing and nacelle stall : results of the closing symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany
وضعیت نشر و پخش و غیره
محل نشرو پخش و غیره
]Cham[
نام ناشر، پخش کننده و غيره
Springer
تاریخ نشرو بخش و غیره
2016
مشخصات ظاهری
نام خاص و کميت اثر
ix, 413 p
فروست
عنوان فروست
Notes on numerical fluid mechanics and multidisciplinary design, 2161-9092 ; volume 131
يادداشت کلی
متن يادداشت
Includes bibliographical references and author index
یادداشتهای مربوط به عنوان و پدیدآور
متن يادداشت
edited by Rolf Radespiel, Reinhard Niehuis, Norbert Kroll, Kathrin Behrends
یادداشتهای مربوط به مسئولیت معنوی اثر
متن يادداشت
The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as presented and discussed by internationally recognized researchers at the Closing Symposium of the DFG Research Unit FOR 1066. Reliable simulations of flow separation on airfoils, wings and powered engine nacelles at high Reynolds numbers represent great challenges in defining suitable mathematical models, computing numerically accurate solutions and providing comprehensive experimental data for the validation of numerical simulations. Additional problems arise from the need to consider airframe-engine interactions and inhomogeneous onset flow conditions, as real aircraft operate in atmospheric environments with often-large distortions. The findings of fundamental and applied research into these and other related issues are reported in detail in this book, which targets all readers, academics and professionals alike, interested in the development of advanced computational fluid dynamics modeling for the simulation of complex aircraft flows with flow separation.
موضوع (اسم عام یاعبارت اسمی عام)
عنصر شناسه ای
، Airplanes -- Wings -- Congresses
عنصر شناسه ای
، Airplanes -- Nacelles -- Congresses
رده بندی کنگره
شماره رده
T
57
.
6
.
S9796
2016
نام شخص به منزله سر شناسه - (مسئولیت معنوی درجه اول )