Aerodynamic performance of an over-the-wing propeller configuration at increasing Mach number

Author:

Müller L.,Kožulović D.,Radespiel R.

Publisher

Springer Science and Business Media LLC

Subject

Aerospace Engineering,Transportation

Reference22 articles.

1. Airbus, S.A.S.: Delivering the Future. Global Market Forecast 2011–2030, Blagnac (2011)

2. Werner-Westphal, C., Heinze, W., Horst, P.: Multidisciplinary integrated preliminary design applied to unconventional aircraft configurations. J. Aircr. 45(2), 581–590 (2008)

3. Müller, L., Heinze, W., Kozulovic, D., Hepperle, M., Radespiel, R.: Aerodynamic installation effects of an over-the-wing propeller on a high-lift configuration. J. Aircr. 51(1), 249–258 (2014)

4. Pasamanick, J.: Langley Full-Scale-Tunnel Tests of the Custer Channel Wing Airplane. NACA Research Memorandum RM L53A09, (1953)

5. Mitchell, K.A.: Mr. Custer and his channel wing airplanes. J. Amer. Aviat. Historical Soc. 43(1), (1998)

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