The F2 wind-tunnel at Fauga-Mauzac

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National Aeronautics and Space Administration , Washington, D.C
Wind tunnels, Aerodyn
Other titlesThe F two wind-tunnel at Fauga-Mauzac
StatementD. Afchain ... [et al.]
SeriesNASA technical memorandum -- 77482
ContributionsAfchain, D, United States. National Aeronautics and Space Administration, Leo Kanner Associates
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL14925293M

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Open Library is an open, editable library catalog, building towards a web page for every book ever published. The F2 wind-tunnel at Fauga-Mauzac Not In Library. Publishing History This is a chart to show the publishing history of editions of works about this subject.

Along the X axis is time, and on the y axis is the count of editions. The present study is devoted to the analysis of the effect of micron-sized roughness elements and of perforated walls on the initial amplitude of the stationary modes developing in a three dimensional boundary layer.

The first part of the paper describes experiments carried out on a swept model in the F2 wind-tunnel at the Fauga-Mauzac ONERA Cited by: 3. We use cookies to offer you a better experience, personalize content, tailor advertising, provide social media features, and better understand the use of our services.

[Show full abstract] in the Onera Fauga- Mauzac F2 wind tunnel. The swept angle was fixed at _ = 40_ for different angles of attack AoA = 5, 6, 7_ and a velocity range varying between 60 and 90 [m/s].Author: Emmanuel Branlard. Full text of "NASA Technical Reports Server (NTRS) Aeronautical engineering: A cumulative index to a continuing bibliography" See other formats.

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Full text of "DTIC ADA Special Course on Fundamentals of Fighter Aircraft Design" See other formats. O Scribd é o maior site social de leitura e publicação do mundo. Control of Vortex Breakdown - Free download as PDF File .pdf), Text File .txt) or read online for free.

This explains the techniques of vortex breakdown. Scribd is the world's largest social reading and publishing site. Space Shuttle wind tunnel testing program. NASA Technical Reports Server (NTRS) Whitnah, A. M.; Hillje, E. A major phase of the Space Shuttle Vehicle (SSV) Developm.

Review of Aeronautical Wind Tunnel Facilities.

Description The F2 wind-tunnel at Fauga-Mauzac EPUB

NASA Technical Reports Server (NTRS) The nation's aeronautical wind tunnel facilities constitute a valuable technologica.

Scribd es red social de lectura y publicación más importante del mundo. ,Attachment Line and Surface Imperfection Problems D. Arnal, J. Perraud and A. Séraudie ONERA/DMAE, Toulouse FRANCE.