Results 41 to 50 of about 15,386 (232)
Abstract Marine stratocumulus clouds (MSC) strongly influence Earth's radiation budget, yet the mechanisms governing the descent of entrainment‐affected (diluted) parcels, and the relative roles of cloud‐top entrainment instability (CTEI) and longwave radiative cooling (RC), remain debated.
Inyeob La +5 more
wiley +1 more source
RESEARCH ON TEST METHOD OF FUSELAGE PANEL SUBJECTED TO INTERNAL PRESSURE LOAD
The test method of fuselage panel subjected to internal pressure load is an important technique for aircraft structure strength research.The constraint simulation technique for the curved and straight boundaries of fuselage panel was studied based on ...
ZANG WeiFeng, DONG DengKe, ZHANG HaiYing
doaj
The subject of the present work is the development and implementation of a novel testing facility to carry out an experimental campaign on an advanced fuselage panel manufactured from both thermoplastic and metallic materials, as well as the validation ...
Panagiotis D. Kordas +2 more
doaj +1 more source
Supersonic aircraft Patent [PDF]
Design of supersonic aircraft with novel fixed, swept wing ...
Carlson, H. W. +4 more
core +1 more source
3D finite element modeling strategy utilizing distal intralaminar cohesive zone (DICZ) and continuum damage mechanics (CDM) for enabling the experimentally validated impact damage in multidirectional composite laminates comprising distal cracks and delamination.
Niildiip Chandraa +5 more
wiley +1 more source
Additive manufacturing (AM) transforms space hardware by enabling lightweight, high‐performance, and on‐demand production. This review outlines AM processes—powder bed fusion (PBF), directed energy deposition (DED), binder jetting (BJ), sheet lamination (SL), and material extrusion (ME)—applied to propulsion, satellite structures, and thermal devices ...
Stelios K. Georgantzinos +8 more
wiley +1 more source
DAMAGE TOLERANCE EXPERIMENT AND ANALYSIS OF STIFFENED FUSELAGE PANEL WITH LONGITUDINAL CRACK
Results from an experimental and analytical study of a curved stiffened aluminum panel subjected to combined internal pressure and axial tension loads are presented.
CHEN An +3 more
doaj
Free wing assembly for an aircraft [PDF]
A free wing is attached to a fuselage of an aircraft in a manner such that the wing is free to pivot about a spanwise axis forward of its aerodynamic center.
Wolowicz, C. H.
core +1 more source
Modified Moment Distribution Method: Rapid Convergence Technique
This paper introduces a Modified Moment Distribution Method (MMDM) to accelerate convergence and enhance computational efficiency in structural analysis. By employing generalized substructures, MMDM reduces iterations while maintaining high accuracy, offering significant improvements over traditional methods. This approach has practical applications in
Mahdi Nouri
wiley +1 more source
Comparing resins with composites, different particle sizes of the flame retardant, and the impact of the flame retardant modes of action on different fire properties. Abstract This study examines the transfer of the flame‐retardant aluminum diethyl phosphinate (AlPi) from epoxy resins to composites and the impact of AlPi on fire behavior and fire ...
Maria Jauregui Rozo +5 more
wiley +1 more source

