NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The role of time-history effects in the formulation of the aerodynamics of aircraft dynamicsThe scope of any aerodynamic formulation proposing to embrace a range of possible maneuvers is shown to be determined principally by the extent to which the aerodynamic indicial response is allowed to depend on the past motion. Starting from the linearized formulation, in which the indicial response is independent of the past motion, two successively more comprehensive statements about the dependence on the past motion are assigned to the indicial response (1) dependence only on the recent past and (2) dependence additionally on a characteristic feature of the distant past. The first enables the rational introduction of nonlinear effects and accommodates a description of the rate-dependent aerodynamic phenomena characteristic of airfoils in low-speed dynamic stall; the second permits a description of the double-valued aerodynamic behavior characteristic of certain kinds of aircraft stall. An aerodynamic formulation based on the second statement, automatically embracing the first, may be sufficiently comprehensive to include a large part of the aircraft's possible maneuvers. The results suggest a favorable conclusion regarding the role of dynamic stability experiments in flight dynamics studies.
Document ID
19790006915
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Tobak, M.
(NASA Ames Research Center Moffett Field, CA, United States)
Schiff, L. B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 10, 2013
Publication Date
November 1, 1978
Publication Information
Publication: AGARD Dyn. Stability Parameters
Subject Category
Aircraft Stability And Control
Accession Number
79N15086
Distribution Limits
Public
Copyright
Other
Document Inquiry

Available Downloads

There are no available downloads for this record.
No Preview Available