Accession Number : AD0753891

Title :   Tragflaechentheorie fuer Tragfluegel mit Strahlklappen (Lifting Surface Theory for Wings with Jet Flaps),

Corporate Author : DEUTSCHE FORSCHUNGSANSTALT FUER LUFT- UND RAUMFAHRT E V BRUNSWICK (WEST GERMANY)

Personal Author(s) : Das,Arabindo

Report Date : 1960

Pagination or Media Count : 24

Abstract : A method for the calculation of the lift distribution of wings of finite span with jet flaps is given. This method is applicable to incompressible flow and is an extension of lifting surface theory of E. Truckenbrodt. Accordingly it can be applied to wings of arbitrary planform (e.g. swept wings and delta wings) with an arbitrary distribution of jet momentum along the span. (Author)

Descriptors :   (*AERODYNAMIC CONTROL SURFACES, *LIFT), JET FLAPS, THEORY, WINGS, INCOMPRESSIBLE FLOW

Subject Categories : Aerodynamics
      Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE