Analytical studies of separated vortex flow on highly swept wings

Download Analytical studies of separated vortex flow on highly swept wings PDF Online Free

Author :
Release : 1978
Genre : Airplanes
Kind :
Book Rating : /5 ( reviews)

Analytical studies of separated vortex flow on highly swept wings - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Analytical studies of separated vortex flow on highly swept wings write by John M. Kuhlman. This book was released on 1978. Analytical studies of separated vortex flow on highly swept wings available in PDF, EPUB and Kindle.

Experimental and Analytical Studies of Separated Vortex Flow on Highly Swept Wings

Download Experimental and Analytical Studies of Separated Vortex Flow on Highly Swept Wings PDF Online Free

Author :
Release : 1977
Genre : Airplanes
Kind :
Book Rating : /5 ( reviews)

Experimental and Analytical Studies of Separated Vortex Flow on Highly Swept Wings - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Experimental and Analytical Studies of Separated Vortex Flow on Highly Swept Wings write by John M. Kuhlman. This book was released on 1977. Experimental and Analytical Studies of Separated Vortex Flow on Highly Swept Wings available in PDF, EPUB and Kindle.

Vortex Flow Behavior Over Slender Delta Wing Configurations

Download Vortex Flow Behavior Over Slender Delta Wing Configurations PDF Online Free

Author :
Release : 2008-10-01
Genre : Science
Kind :
Book Rating : 326/5 ( reviews)

Vortex Flow Behavior Over Slender Delta Wing Configurations - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Vortex Flow Behavior Over Slender Delta Wing Configurations write by Xing Z. Huang. This book was released on 2008-10-01. Vortex Flow Behavior Over Slender Delta Wing Configurations available in PDF, EPUB and Kindle. The book discusses the behavior of vortices over sharp and highly swept wing configurations used for current and future military aircraft. Special attention is paid to the effects of critical flow phenomenon such as vortex breakdown occuring at high angles of attack or high angular rates. The wind tunnel experiments conducted on delta-wing configurations in wind tunnels in Canada, Europe, Russia and the United States are given in eight chapters. The experiments provide an extended data base that gives insight into the effects of the angle of attack, angular rate, Reynolds number and Mach number on the behavior of vortices over several slender delta wings in stationary and instationary flights. A critical assessment is given in a separated chapter of the available experimental data bases and out of these data, one and the same data set is selected for the validation and verification of analytical and numerical solutions.Comprehansive computational results are given in another ten chapters. Steady-state and time-accurate solutions for the steady and unsteady flow over the selected delta-wing configuration are discussed. These solutions are generated using structured and unstructured grid methods.The analytical solutions for the flow over a delta wing are discussed and compared with experimental data in three more chapters.In the final chapter a validation and verification of the analytical and CFD solutions is given.

Separation Ahead of Controls on Swept Wings

Download Separation Ahead of Controls on Swept Wings PDF Online Free

Author :
Release : 1975
Genre : Aerodynamics, Hypersonic
Kind :
Book Rating : /5 ( reviews)

Separation Ahead of Controls on Swept Wings - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Separation Ahead of Controls on Swept Wings write by Kaufman Louis G. (II). This book was released on 1975. Separation Ahead of Controls on Swept Wings available in PDF, EPUB and Kindle. Shock-induced flow-separation ahead of trailing edge controls on swept wings is investigated with emphasis on the effects of boundary layer transition on the location and shape of the separation line. Experimental results were obtained by using forward facing steps mounted on swept-leading-edge flat-plate wing models in the ARL Mach 6 Tunnel for model running length Reynolds numbers varying from 0.9 to 33 million. The data support qualitatively a proposed, strip-type method for estimating, the extent and shape of the three dimensional region of separated flow ahead of controls on swept wings. (Author).

Scientific and Technical Aerospace Reports

Download Scientific and Technical Aerospace Reports PDF Online Free

Author :
Release : 1976
Genre : Aeronautics
Kind :
Book Rating : /5 ( reviews)

Scientific and Technical Aerospace Reports - read free eBook in online reader or directly download on the web page. Select files or add your book in reader. Download and read online ebook Scientific and Technical Aerospace Reports write by . This book was released on 1976. Scientific and Technical Aerospace Reports available in PDF, EPUB and Kindle.