Results of boundary-layer investigations on the leeward side of a 1: 12 scale model of the ELAC 1 configuration of a space transportation system are presented. The configuration has the shape of a thick delta wing with a rounded leading edge. The model length is 6 m; the experiments were carried out
β¦ LIBER β¦
An experimental investigation of the ELAC 1 configuration at supersonic speeds
β Scribed by E. Krause; W. Limberg; A. M. Kharitonov; M. D. Brodetsky; A. Henze
- Publisher
- Springer
- Year
- 1999
- Tongue
- English
- Weight
- 800 KB
- Volume
- 26
- Category
- Article
- ISSN
- 0723-4864
No coin nor oath required. For personal study only.
π SIMILAR VOLUMES
Boundary-layer investigations on a model
β
Egon Krause; Ronald Abstiens; Stefan FΓΌhling; Vitali N. Vetlutsky
π
Article
π
2000
π
Elsevier Science
π
English
β 693 KB
Experimental investigation of local heat
β
N. F. Ragulin; Yu. G. Shvalev
π
Article
π
1983
π
Springer US
π
English
β 307 KB
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
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
Experimental investigation of the intera
β
A. I. Shvets
π
Article
π
1983
π
Springer
π
English
β 742 KB
An experimental investigation of the noz
β
V. I. Zapryagaev; A. V. Solotchin
π
Article
π
1997
π
SP MAIK Nauka/Interperiodica
π
English
β 734 KB
Investigation of the supersonic flow aro
β
V. N. Vetlutskii; V. L. Ganimedov
π
Article
π
1976
π
SP MAIK Nauka/Interperiodica
π
English
β 485 KB