✦ LIBER ✦

Large injection rates on unsteady compressible boundary layer flow over cones at angles of attack

✍ Scribed by A. Sau

Book ID: 120900254
Publisher: Springer
Year: 1995
Tongue: English
Weight: 394 KB
Volume: 65
Category: Article
ISSN: 0939-1533
DOI: 10.1007/BF00787533

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Experimental study of compressible bound

Experimental study of compressible boundary layer on a cone at angles of attack

✍ A. Maslov; D. Bountin; A. Shiplyuk; A. Sidorenko; Q. Shen; Z. Bi 📂 Article 📅 2009 🏛 The Chinese Society of Theoretical and Applied Mec 🌐 English ⚖ 870 KB

Laminar Boundary Layer on a Spinning Con

Laminar Boundary Layer on a Spinning Cone at Small Angles of Attack in a Supersonic Flow

✍ SEDNEY, R. 📂 Article 📅 1957 🏛 American Institute of Aeronautics and Astronautics ⚖ 776 KB

Effect of asymmetry of the boundary cond

Effect of asymmetry of the boundary conditions on the boundary layer flow near a cone at an angle of attack

✍ E. S. Kornienko; V. M. Shuchinov 📂 Article 📅 1989 🏛 Springer 🌐 English ⚖ 379 KB

Effect of large blowing rates on the com

Effect of large blowing rates on the compressible boundary layer flow at the stagnation point of a rotating sphere

✍ M. Kumari; G. Nath 📂 Article 📅 1997 🏛 Springer Vienna 🌐 English ⚖ 745 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 25th AIAA Aerospace Sciences Meeting - Reno,NV,U.S.A. (24 March 1987 - 26 March 1987)] 25th AIAA Aerospace Sciences Meeting - The stability of the compressible boundary layer on a sharp cone at zero angle of attack

✍ GASPERAS, G. 📂 Article 📅 1987 🏛 American Institute of Aeronautics and Astronautics ⚖ 446 KB