Accession Number:

AD0733597

Title:

Zur Stabilitaet des schwingenden Tragfluegels im Unterschallbereich (Stability of an Oscillating Wing in Subsonic Range),

Descriptive Note:

Corporate Author:

DEUTSCHE FORSCHUNGS- UND VERSUCHSANSTALT FUER LUFT- UND RAUMFAHRT E V FREIBURG IM BREISGAU (WEST GERMANY)

Personal Author(s):

Report Date:

1969-01-01

Pagination or Media Count:

9.0

Abstract:

An oscillating wing with control surfaces in two-dimensional, compressible, subsonic flow is investigated. Computed numerical results are given for the forces and moments, useful for flutter calculations.

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE