Description of FLO22 code written for solution of transonic flow past a swept wing

Download

008177.pdf

Date

1990

Author

Yağcı, Hüseyin

Metadata

Show full item record

Item Usage Stats

123
views

0
downloads

URI

https://hdl.handle.net/11511/3808

Collections

Graduate School of Natural and Applied Sciences, Thesis

Suggestions

OpenMETU
Core

Description of BIST 50 via volatility models and sector-based variables Purutçuoğlu Gazi, Vilda (null; 2019-11-01)
Description of LMARS model under StARS model selection criterion in the description of biological networks Bülbül, Gül Bahar; Purutçuoğlu Gazi, Vilda (null; 2019-07-12)
Description of the PM process by using Ishikawa-analysis Simon, Andrea; Kovács, Károly; Gür, Cemil Hakan; Pieczonka, Tadeusz; Gácsi, Zoltán (2013-01-01) Composites are special materials which can provide specific individual properties such as high strength with low density or good thermal conductivity with low thermal expansion coefficient. Composites follow the constantly evolving and more complex expectations. In order to make a product with good quality, it is important to choose suitable materials and technology. In this research, powder metallurgy (PM), as one of the most common composite manufacturing technologies, was examined; which factors and mech...
Description of Barely Transitive Groups with Soluble Point Stabilizer Betin, Cansu; Kuzucuoğlu, Mahmut (Informa UK Limited, 2009-6-4) We describe the barely transitive groups with abelian-by-finite, nilpotent-by-finite and soluble-by-finite point stabilizer. In article [6] Hartley asked whether there is a torsionfree barely transitive group. One consequence of our results is that there is no torsionfree barely transitive group whose point stabilizer is nilpotent. Moreover, we show that if the stabilizer of a point is a permutable subgroup of an infinitely generated barely transitive group G, then G is locally finite.
Description of the System with Fixed Moments of Impulses and Its Solutions Akhmet, Marat (2010-01-01)

Citation Formats

H. Yağcı, “Description of FLO22 code written for solution of transonic flow past a swept wing,” Middle East Technical University, 1990.