✦ LIBER ✦

Investigation of a ‘transonic resonance’ with convergent–divergent nozzles

✍ Scribed by ZAMAN, K. B. M. Q.; DAHL, M. D.; BENCIC, T. J.; LOH, C. Y.

Book ID: 120116760
Publisher: Cambridge University Press
Year: 2002
Tongue: English
Weight: 493 KB
Volume: 463
Category: Article
ISSN: 0022-1120
DOI: 10.1017/S0022112002008819

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Experimental investigation on noise supp

Experimental investigation on noise suppression in supersonic jets from convergent-divergent nozzles with baffles

✍ Yoshiaki Miyazato; Yong-Hun Kweon; Toshiyuki Aoki; Mitsuharu Masuda; Kwon-Hee Le 📂 Article 📅 2003 🏛 Springer-Verlag 🌐 English ⚖ 460 KB

Metering characteristics of a convergent

Metering characteristics of a convergent-divergent nozzle with a cylindrical throat

✍ N. L. Efremov 📂 Article 📅 1993 🏛 Springer 🌐 English ⚖ 129 KB

Flashing Flow of Initially Subcooled Wat

Flashing Flow of Initially Subcooled Water in Convergent–Divergent Nozzles

✍ Schrock, V. E.; Starkman, E. S.; Brown, R. A. 📂 Article 📅 1977 🏛 The American Society of Mechanical Engineers 🌐 English ⚖ 537 KB

A remark on determination of transonic s

A remark on determination of transonic shocks in divergent nozzles for steady compressible Euler flows

✍ Hairong Yuan 📂 Article 📅 2008 🏛 Elsevier Science 🌐 English ⚖ 190 KB

Simulation of cavitation bubbles in a co

Simulation of cavitation bubbles in a convergent–divergent nozzle water jet

✍ QIN, Z.; BREMHORST, K.; ALEHOSSEIN, H.; MEYER, T. 📂 Article 📅 2007 🏛 Cambridge University Press 🌐 English ⚖ 334 KB

Heat transfer of gas-particle flow in a

Heat transfer of gas-particle flow in a supersonic convergent-divergent nozzle

✍ Wazzan, A. R. ;Robinson, L. B. ;Diem, H. G. 📂 Article 📅 1968 🏛 Springer 🌐 English ⚖ 962 KB

H e a t flux, wall heat transfer coefficients, and wall pressures are determined for high velocity flow of gas-solid mixtures in a converging-diverging nozzle. Flow separation accompanied with oblique shock formation occurs in the diverging section of the nozzle. The shock strength is reduced upon t