Accession Number:

AD0642156

Title:

ON CERTAIN TYPES OF SELF-EXCITED OSCILLATION OCCURRING WITH AIRCRAFT CONTROL SURFACES IN TRANSONIC FLOW,

Descriptive Note:

Corporate Author:

NATIONAL PHYSICAL LAB TEDDINGTON (ENGLAND) AERODYNAMICS DIV

Personal Author(s):

Report Date:

1966-02-21

Pagination or Media Count:

15.0

Abstract:

Brief reference is made to the results of wind-tunnel experiments on self-excited oscillations of control surfaces in transonic flow. Two particular examples are discussed and an attempt is made to provide theoretical mechanisms of oscillation which are in agreement with the observations. Author

Subject Categories:

  • Aircraft
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE