Calculation of Jet Aircraft Parameters Under Design Requirements TsAGI

Format:

Conference/Event

Author/Creator:

Bashkirov, I.G., author.

Conference Name:

World Aviation Congress & Exposition (1997-10-13 : Anaheim, California, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1997

Summary:

This paper presents a method for preliminary aircraft design at initial determination of aircraft dimension, weight, thrust and aerodynamics under specified flight-performance requirements (FPR). The main flight-performance are:Achieving required supersonic Mach number at specified engine operating mode and at specific excess power can be considered as additional FPR.The idea of the method is to transfer the FPR into requirements to aircraft dimension, weight, thrust and aerodynamics. The method is based on relation between aircraft energy possibilities and it's arrangement parameters, "mass-geometry" and "geometry-aerodynamics" relations in a form of analytical equations.Simplicity and rapidity of technique application make it suitable for use at preliminary design

Notes:

Vendor supplied data

Publisher Number:

975598

Access Restriction:

Restricted for use by site license