Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb-Reference-Cited by-同舟云学术

Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb

Published:2017-09-19 Issue:4 Volume:8 Page:613-623
ISSN:1869-5582
Container-title:CEAS Aeronautical Journal
language:en
Short-container-title:CEAS Aeronaut J

Author:

Weiss Armin^ORCID,Gardner Anthony D.,Klein Christian,Raffel Markus

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Link

http://link.springer.com/article/10.1007/s13272-017-0263-2/fulltext.html

Reference43 articles.

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2. Egolf, T.A., Hariharan, N., Narducci, R., Reed, E.: AIAA standardized hover simulation: hover performance prediction status and outstanding issues. In: 55th AIAA Aerospace Sciences Meeting, AIAA 2017-1429. Grapevine, Texas (2017). doi: 10.2514/6.2017-1429

3. Schubauer, G.B., Skramstad, H.K.: Laminar boundary-layer oscillations and stability of laminar flow. J. Aeronaut. Sci. 14(2), 69–78 (1947). doi: 10.2514/8.1267

4. Bass, R.M.: Small scale wind tunnel testing of model propellers. In: 24th Aerospace Sciences Meeting. Reno, Nevada (1986). doi: 10.2514/6.1986-392

5. McCroskey, W.J.: Measurements of boundary layer transition, separation and streamline direction on rotating blades. Tech. Rep. TN D-6321, NASA (1971)

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