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A Wing-by-Wing Approach for Biplane Static Longitudinal Stability and Control Analysis

SAE Technical Paper Series, 2008
<div class="htmlview paragraph">This paper presents a theoretical model for the analysis of the longitudinal static stability and control of biplane aircrafts that take into account some effects neglected by the classical approach based on the concept of an aerodynamically equivalent monoplane.
Westin, Michelle Fernandino   +1 more
openaire   +1 more source

A New Method of Strengthening Longitudinal Static Stability of Airship in Ascent

Applied Mechanics and Materials, 2014
To improve the controllability and maneuverability, airship is usually designed as static instability. But the airship is vulnerable to sudden wind interference in its ascent, resulting in divergent pitching motion. A new aerodynamic shape was put forward which added a inflatable aerodynamic-lift wing at backward of the airship hull. With the method of
Hou Di Xiao   +3 more
openaire   +1 more source

Low speed longitudinal aerodynamic, static stability and performance analysis of a hypersonic waverider

Aerospace Science and Technology, 2020
Abstract Hypersonic waveriders have the potential to significantly reduce travel times on long haul civilian transport routes. The design of hypersonic aircraft is heavily influenced by the aerodynamic efficiency at the cruise Mach number, resulting in less than ideal geometries for subsonic flight.
Tamas Bykerk   +2 more
openaire   +1 more source

The theory of the longitudinal static stability of the hang-glider

The Aeronautical Journal, 1994
AbstractThis paper describes the development of a simple theory of the longitudinal static stability of the hang-glider. The classical theory, as developed for the conventional aeroplane, is modified to accommodate the particular features of the hang-glider. When the appropriate assumptions are made, the theory provides simple insight into the controls
openaire   +1 more source

Effect of Upper-Surface Blowing on Static Longitudinal Stability of a Swept Wing

Journal of Aircraft, 1974
A low-speed wind-tunnel investigation was conducted on a sharp-edged 75 deg delta wing, to determine the effect of upper-surface blowing on static longitudinal stability characteristics. The model incorporated nozzles, located at 0.50 mean aerodynamic chord length, supplied by compressed air to provide blowing on the upper surface.
Paul L. Coe, D. Kulla
openaire   +1 more source

Main static aeroelastic effects on sailplane longitudinal stability and control

1976
In the paper the effects of the wing torsional deformation and of the fuselage bending deformation are considered, as being probabily the most important ones. The classical theoretical expressions for equilibrium and stability are therefore modified, in order to take into account these aeroelastic effects, and discussed.
NUCCIO, Patrizio, Piero Morelli
openaire   +1 more source

Dynamic and reconfigurable materials from reversible network interactions

Nature Reviews Materials, 2022
Matthew J Webber, Mark W Tibbitt
exaly  

The stiffness of living tissues and its implications for tissue engineering

Nature Reviews Materials, 2020
Carlos F GuimarĂ£es   +2 more
exaly  

Exploiting the paddle-wheel mechanism for the design of fast ion conductors

Nature Reviews Materials, 2022
Zhizhen Zhang, Linda F Nazar
exaly  

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