Shabeer et al., 2013 - Google Patents
Optimization of aircraft wing with composite materialShabeer et al., 2013
View PDF- Document ID
- 7057368176139564993
- Author
- Shabeer K
- Murtaza M
- Publication year
- Publication venue
- International Journal of Innovative Research in Science, Engineering and Technology
External Links
Snippet
The objective of this paper is to develop an accurate model for optimal design through design the structure of wing that combine the composite (Skins) and isotropic materials (all other structures) and compare this with the same wing made by changing the orientation of …
- 239000002131 composite material 0 title abstract description 20
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
- Y02T50/42—Airframe
- Y02T50/43—Materials
- Y02T50/433—Composites
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
- B64C1/064—Stringers; Longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/18—Spars; Ribs; Stringers
- B64C3/182—Stringers, longerons
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/26—Construction, shape, or attachment of separate skins, e.g. panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/32—Rotors
- B64C27/46—Blades
- B64C27/473—Constructional features
- B64C2027/4733—Rotor blades substantially made from particular materials
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/44—Varying camber
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Shabeer et al. | Optimization of aircraft wing with composite material | |
Castanie et al. | Review of composite sandwich structure in aeronautic applications | |
Guo | Aeroelastic optimization of an aerobatic aircraft wing structure | |
Dillinger et al. | Static aeroelastic stiffness optimization and investigation of forward swept composite wings | |
Rajappan et al. | Finite element analysis of aircraft wing using composite structure | |
Bramsiepe et al. | Loads and structural optimization process for composite long range transport aircraft configuration | |
Rajadurai et al. | Optimization of ply orientation of different composite materials for aircraft wing | |
Bach et al. | Structural optimization of composite wings in an automated multi-disciplinary environment | |
Park et al. | Structural analysis of a composite target-drone | |
Garre et al. | Modeling and analysis of a RIBS and Spars of an airplane wing for bending and shear loads | |
Murugan et al. | Morping helicopter rotor blade with curvilinear fiber composites | |
Akshayraj et al. | Design and analysis of a tail sitter (VTOL) UAV composite wing | |
Prabhu et al. | Optimization of unmanned aerial vehicle wing structure | |
Moore et al. | Structural design exploration of an electric powered multi-propulsor wing configuration | |
Kirubakaran et al. | Aircraft wing weight optimization by composite material structure design configuration | |
Ramos | Construction and analysis of a lightweight UAV wing prototype | |
Grodzki et al. | Modelling of UAV's composite structures and prediction of safety factor | |
Pareja Muñoz | Study and design of a wing monocoque structure with composite materials | |
Papapetrou et al. | Preliminary Wing Study of General Aviation Aircraft with Stitched Composite Panels | |
Bourchak et al. | Design and analysis of a morphing composite airfoil using unbalanced layup and unconventional ply angles | |
Jamil et al. | Fluid Coupled Structural Analysis and Optimization of Expanded Polystyrene-Fiber-Reinforced Composite Wing of an Unmanned Aerial Vehicle | |
Kumar et al. | DESIGN AND STRESS ANALYSIS OF SWEPT BACK WING WITH NASTRAN AND PATRAN | |
Tahir et al. | Performance evaluation of unmanned aerial vehicle wing made from sterculiasetigeradelile fiber and pterocarpuserinaceus wood dust epoxy composite using finite element method abaqus and structural testing | |
Lim et al. | Structural integrity design of a composite wing in a tiltrotor aircraft | |
Sommerwerk et al. | Influence of engine modeling on structural sizing and approach aerodynamics of a circulation controlled wing |