An experiment was conducted on a two-dimensional bifurcated, supersonic inlet to investigate the aeroacoustics at take-o! and landing conditions. A 104)1 mm (4)1 in) diameter turbofan simulator was coupled to the inlet to generate the noise typical of a turbofan engine. Aerodynamic and acoustic data
β¦ LIBER β¦
Investigation of the pseudo-shock wave in a two-dimensional supersonic inlet
β Scribed by Hyoung Jin Lee; Bok Jik Lee; Sung Don Kim; In-Seuck Jeung
- Book ID
- 107680075
- Publisher
- IOS Press
- Year
- 2009
- Tongue
- English
- Weight
- 475 KB
- Volume
- 13
- Category
- Article
- ISSN
- 1343-8875
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
AN EXPERIMENTAL INVESTIGATION OF THE AER
β
S.-M. LI; C.A. HANUSKA; W.F. NG
π
Article
π
2001
π
Elsevier Science
π
English
β 501 KB
Investigation of separated flow behind t
β
A. N. Ivanov; V. I. Mikhailov
π
Article
π
1985
π
SP MAIK Nauka/Interperiodica
π
English
β 799 KB
Investigation of the closing shock in a
β
V. I. Nemchenko
π
Article
π
1971
π
Springer US
π
English
β 811 KB
The stability of a metastable shock wave
β
A.G. Kulikovskii; A.P. Chugainova
π
Article
π
2002
π
Elsevier Science
π
English
β 859 KB
The unsteady motions of a viscoelastic medium are considered, taking account of a small anisotropy and a small non-linearity. The behaviour of a metastable, quasi-transverse shock wave when it interacts with non-one-dimensional perturbations is investigated numerically. The stability of this wave un
Investigation of the properties of a sho
β
S. G. Zaitsev; A. V. Mikhailov; I. K. Favorskaya
π
Article
π
1976
π
Springer
π
English
β 653 KB
The effect of MHD interactions on the in
β
S. V. Bobashev; R. V. Vasilβeva; E. A. Dβyakonova; A. V. Erofeev; T. A. Lapushki
π
Article
π
2001
π
SP MAIK Nauka/Interperiodica
π
English
β 63 KB