Boundary Layer Studies On A Spinning Cone
Download Boundary Layer Studies On A Spinning Cone full books in PDF, epub, and Kindle. Read online free Boundary Layer Studies On A Spinning Cone ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Author | : Walter B. Sturek |
Publisher | : |
Total Pages | : 58 |
Release | : 1973 |
Genre | : Boundary layer |
ISBN | : |
An experimental investigation of the effects of spin induced distortion of the boundary layer on a spinning 10 degree half angle cone at Mach 2, 3 and 4 is reported. The profile of the location of boundary layer transition has been determined completely about the surface of the cone model from spark shadowgraphs. These spark shadowgraphs were taken with the model mounted on an offset strut which was rolled incrementally in azimuth to reveal the entire surface of the model. The profile of the boundary layer thickness at the base of the cone has also been determined from the spark shadowgraphs. Strain gage balance measurements of Magnus and normal force were made for three significantly different boundary layer configurations and confirm the extreme sensitivity of Magnus to boundary layer configuration.
Author | : Walter B. Sturek |
Publisher | : |
Total Pages | : 52 |
Release | : 1975 |
Genre | : Boundary layer |
ISBN | : |
An experimental investigation of the Magnus effect on a seven caliber tangent-ogive-cylinder model in supersonic flow is reported. The effects of surface spin, angle of attack and Mach number on boundary-layer transition have been studied using spark shadowgraphs of the flow. These shadowgraphs were taken while the model was mounted on offset struts to enable views to be obtained of the flow completely about the circumference of the model. The Magnus and normal forces were measured using the strain-gage balance technique for different boundary layer configurations. These measurements revealed a substantial sensitivity of Magnus force to the boundary layer configuration. A preliminary comparison of the Magnus measurements to the theory of Vaughn and Reis yielded poor agreement. The data have been tabulated to facilitate their use in the evaluation of proposed theoretical models of the Magnus effect.
Author | : Walter B. Sturek |
Publisher | : |
Total Pages | : 34 |
Release | : 1974 |
Genre | : Body of revolution |
ISBN | : |
An experimental investigation of the effects of spin induced distortion of the boundary-layer on a spinning cone and tangent-ogive-cylinder model for small angle of attack at Mach 2, 3 and 4 is reported. The profile of the location of boundary-layer transition has been determined completely about the surface of the models from spark shadowgraphs. These spark shadowgraphs were taken with the model mounted on an offset strut which was rolled incrementally in azimuth to reveal the entire surface of the model. Strain gage balance measurements of Magnus and normal force were made for three significantly different boundary-layer configurations--predominately laminar, predominately turbulent, tripped to turbulent--and confirm the pronounced sensitivity of Magnus to boundary-layer configuration. (Author).
Author | : Hans U. Meier |
Publisher | : Springer Science & Business Media |
Total Pages | : 512 |
Release | : 2012-12-06 |
Genre | : Science |
ISBN | : 3642829945 |
The present volume entitled "Perspectives in Turbulence Stud ies" is dedicated to Dr. Ing. E. h. Julius C. Rotta in honour of his 75th birthday. J. C. Rotta, born on January 1, 1912, started his outstanding career in an unusual way, namely in a drawing office (1928 - 1931). At the same time he - as a purely self taught perso- took a correspondence course in airplane construction. From 1934 to 1945 he worked in the aircraft industry on different subjects in the fields of flight mechanics, structures, air craft design, and aerodynamics. In 1945 he moved to Gottingen and worked from that time at the Aerodynamische Versuchsanstalt (AVA, now DFVLR) and the Max-Planck-Institut fur Stromungsforschung (1947-1958), interrupted only by a stay in the U. S. at the Glenn L. Martin Company (1954 - 1955) and a visiting professorship at the Laval University in Quebec, Canada (1956). Already during his activities in industry, Dr. Rotta discovered his special liking for aerodynamics. In Gottingen, he was attracted by Ludwig Prandtl's discussions about problems associated with turbulence and in particular his new contribution to fully developed turbulence, published in 1945. At that time, W. Heisenberg and C. F. v. Weizacker pub lished their results on the energy spectra of isotropic turbu lence at large wave numbers. Since that time his main research interest in reasearch has been in turbulence problems.
Author | : |
Publisher | : |
Total Pages | : 730 |
Release | : 1980 |
Genre | : Aeronautics |
ISBN | : |
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Author | : |
Publisher | : |
Total Pages | : 350 |
Release | : 1963 |
Genre | : Research |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 1000 |
Release | : 1974 |
Genre | : Research |
ISBN | : |
Author | : |
Publisher | : |
Total Pages | : 592 |
Release | : 1974 |
Genre | : Mechanics, Applied |
ISBN | : |
Author | : United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch |
Publisher | : |
Total Pages | : 1080 |
Release | : 1985 |
Genre | : Science |
ISBN | : |
Author | : H. R. Vaughn |
Publisher | : |
Total Pages | : 70 |
Release | : 1973 |
Genre | : Body of revolution |
ISBN | : |
An analysis is presented for predicting Magnus force and moment coefficients for spinning ogive cylinder, cone cylinder, and conical bodies with laminar, transitional and turbulent boundary layers. The results compare favorably with experimental data.