Author : R. W. Butler
Publisher :
Page : 60 pages
File Size : 13,33 MB
Release : 1976
Category : Damping (Mechanics).
ISBN :
An investigation was conducted to provide some insight into the importance of dynamic cross and cross-coupling derivatives in motion simulation studies of fighter aircraft in the maneuvering flight regime. The aircraft motion sensitivity to the various derivatives is ascertained in level and turning flight utilizing a 5 deg of freedom linearized stability program. The results are presented in a root locus format.
Author : T. F. Langham
Publisher :
Page : 146 pages
File Size : 50,47 MB
Release : 1980
Category : Angle of attack (Aerodynamics)
ISBN :
Author :
Publisher :
Page : 702 pages
File Size : 21,48 MB
Release : 1995
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 818 pages
File Size : 36,81 MB
Release : 1979
Category : Aerodynamics
ISBN :
Author : T. F. Langham
Publisher :
Page : 116 pages
File Size : 18,88 MB
Release : 1980
Category : Guided missiles
ISBN :
A dynamic derivative sensitivity study was conducted to demonstrate the importance of dynamic derivatives in missile motion simulation studies. Generalized bank-to-turn and yaw-to-turn missile configurations were used with a six-degree-of-freedom linearized stability program. The effects of various dynamic derivatives on missile stability were investigated in both level and turning flight for several Mach numbers and altitude conditions.
Author :
Publisher :
Page : 142 pages
File Size : 39,51 MB
Release : 1980
Category : Aeronautics
ISBN :
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA)
Author :
Publisher :
Page : 356 pages
File Size : 36,72 MB
Release : 1983
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 996 pages
File Size : 28,62 MB
Release : 1984
Category : Government reports announcements & index
ISBN :
Author : K. S. Keen
Publisher :
Page : 236 pages
File Size : 48,34 MB
Release : 1996
Category : Equations of motion
ISBN :
The mathematical equations of motion for ground simulation of the separation trajectories of stores from aircraft are developed in this document. The equations have application to both analytical and wind tunnel captive trajectory store separation testing. The equations of motion as presented here include features not previously available in AEDC analytical and wind tunnel simulations such as arbitrary aircraft maneuvers, more rigorous models of the specific pivot hardware used by some aircraft, and downrail motions with all components of kinematic acceleration (including Corlolis effects) modeled. The data reduction equations for free-falling instrumented store models are also included.
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher :
Page : 542 pages
File Size : 50,68 MB
Release : 1984
Category : Aeronautics
ISBN :
