COMPLIANT WALL, SUPERSONIC WIND TUNNEL.
Publication
, Journal Article
Dowell, EH
Published in: Aeronaut J
January 1, 1978
The concept of a self-correcting wind tunnel with impermeable flexible walls deformed into an a priori determined shape of fixed magnitude is broadened to allow at least the magnitude of the wall shape to vary with flow conditions, e. g. , flow dynamic pressure. The compliant wall is then modeled as rigid hinged segments whose compliance is determined by attached springs. This concept allows for a much wider range of flow regimes and compliant wall characteristics at the cost of some increased complexity in mathematics.
Duke Scholars
Published In
Aeronaut J
ISSN
0001-9240
Publication Date
January 1, 1978
Volume
82
Issue
814
Start / End Page
448 / 451
Related Subject Headings
- Aerospace & Aeronautics
- 15 Commerce, Management, Tourism and Services
- 09 Engineering
Citation
APA
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ICMJE
MLA
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Dowell, E. H. (1978). COMPLIANT WALL, SUPERSONIC WIND TUNNEL. Aeronaut J, 82(814), 448–451.
Dowell, E. H. “COMPLIANT WALL, SUPERSONIC WIND TUNNEL.” Aeronaut J 82, no. 814 (January 1, 1978): 448–51.
Dowell EH. COMPLIANT WALL, SUPERSONIC WIND TUNNEL. Aeronaut J. 1978 Jan 1;82(814):448–51.
Dowell, E. H. “COMPLIANT WALL, SUPERSONIC WIND TUNNEL.” Aeronaut J, vol. 82, no. 814, Jan. 1978, pp. 448–51.
Dowell EH. COMPLIANT WALL, SUPERSONIC WIND TUNNEL. Aeronaut J. 1978 Jan 1;82(814):448–451.
Published In
Aeronaut J
ISSN
0001-9240
Publication Date
January 1, 1978
Volume
82
Issue
814
Start / End Page
448 / 451
Related Subject Headings
- Aerospace & Aeronautics
- 15 Commerce, Management, Tourism and Services
- 09 Engineering