Investigation of Lifting Properties of the Fuselage Constructed by Airfoils with Air Extraction at the Upper Critical Point for a Short Take-Off and Landing Air Taxi

Author:

Mel’nikova A. I.,Kuznetsov P. N.,Bulat M. P.

Publisher

Allerton Press

Subject

Aerospace Engineering

Reference24 articles.

1. Wick, A.T., Hooker, J.R.. Hardin, C.J.. and Zeune, C.H., Integrated Aerodynamic Benefits of Distributed Propulsion, Proc. of the AIAA 53rd Aerospace Sciences Meeting, 2015, Kissimmee, USA, AIAA Paper no. 2015–1500.

2. Petrov, A.V., Aerodinamika transportnykh samoletov korotkogo vzleta i posadki s energeticheskimi sistemami uvelicheniya pod'emnoi sily (Aerodynamics of Short Takeoff and Landing Transport Aircraft with Energy Methods for Increasing Lift), Moscow: Innovatsionnoe Mashinostroenie, 2018.

3. Kornev, A.V., Sereda, V.A., and Migalin, K.V., Aerodynamic Design Method of Integrated Aircraft with Submerged Intake Devices and Power Plant Included into Airframe Carrying System, Izv. Vuz. Av. Tekhnika, 2018, vol. 61, no. 1, pp. 17–25 [Russian Aeronautics (Engl. Transl.), vol. 61, no. 1, pp. 14–22].

4. NASA's X-57 Electric Research Plane, URL: https://www.nasa.gov/image-feature/nasas-x-57-electric-research-plane.

5. Giannini, F., et al., US Patent 2017/0203839, 2017.

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