DECREASE OF SOUND PRESSURE LEVEL AND NOISE INSIDE HYBRID ELECTRIC WING BODY PLANES AND DIRIDGABLES

Volume 5, Issue 4, August 2020     |     PP. 80-90      |     PDF (285 K)    |     Pub. Date: August 12, 2020
DOI:    215 Downloads     2698 Views  

Author(s)

Prof. Mikhail KUPRIKOV, Moscow Aviation Institute, Moscow, Russia
Dr. Leonid PONYAEV, Moscow Aviation Institute, Moscow, Russia
Dr. Nikita KUPRIKOV, Moscow Aviation Institute, Moscow, Russia

Abstract
The analysis of the find Optimal Structure of the Large Aircraft and Airship for decrease of Sound/Noise Pressure Level inside and outside the Cabin Saloon are very actually today for Worldwide Ecology Program. The Method of Aircraft layout from the virtual mass center is given, which allows us to obtain the Aircraft layout from the conditions of Infrastructural Constraints in the terminal configurations of the Modern Air Transportation Infrastructure and IATA/ICAO Regulation. A Method is proposed for the synthesis of new circuit solutions for an Aircraft passenger compartment and may be use to any Diridgables Projections future. A Geometrical representation of the concept of LHA with large passenger capacity made with a Drop-Shaped Fuselage in the Aerodynamic balancing Flying Wing Body Scheme is given. The new Body Plane LHA and Lighter-then-Air (LTA) Vehicles with cover of Solar Electro Systems will be more innovation projections for Worldwide Security Air Transportation with reduce Noise and CO Pollution Level.

Keywords
aircraft, bodywing, airship, solar, structure, sound, noise

Cite this paper
Prof. Mikhail KUPRIKOV, Dr. Leonid PONYAEV, Dr. Nikita KUPRIKOV, DECREASE OF SOUND PRESSURE LEVEL AND NOISE INSIDE HYBRID ELECTRIC WING BODY PLANES AND DIRIDGABLES , SCIREA Journal of Physics. Volume 5, Issue 4, August 2020 | PP. 80-90.

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