Add to ORKGIn this report, a description of finite element modelling strategy for Static Analysis of Rotodomed Aircraft using Automatic Multi-Stage Substructuring(AMSS)capability in CSA/NASTRAN software package has been presented. Individual components of AEW system like Fuselage, Pylon and Deckplate have been identified as substructures. The substructue models have been verified through simple analysis checks. The results of the analysis under realistic loads will be provided in the subsequent parts of the report
This paper introduces a fully parameterized finite element based tool chain for the structural sizin...
The NASTRAN model plan for the fairing structure was expanded in detail to generate the NASTRAN mode...
The development of a structural finite element model for a generic transonic transport is presented....
Numerical results from a finite element analysis of rotodomed aircraft are presented. Automatic Mult...
Static Analysis of Rotodomed Aircra.t teas, been carries out usi Automatic Multistage Substructure (...
Stress analysis of an assemblage of HS-748 fuselage,\ud pylons and platform is carried out employing...
pCRM9 aeroelastic aircraft wing model for NASTRAN without RBE2 Based on the model published by Paul...
The use of NASTRAN at Bell Helicopter Company for structural static and dynamic analysis of a helico...
An application of NASTRAN to the structural analysis of light aircraft was conducted to determine th...
Stress analysis of metallic rudder of MiG-21 is carried out by finite element technique using the so...
This report contains the details of finite element analysis of radome for Mirage 2000. The radome is...
The objective of static testing of metallic rudder was to determine its sparline and trailing edge d...
The mathematical models and data used in the off-line flight simulation of the rotodomed aircraft ha...
The fuselage is an airplane’s main body section that holds crew and passengers. The design of a fuse...
The development of new air- and rotorcraft is very challenging. The design process is divided into t...
This paper introduces a fully parameterized finite element based tool chain for the structural sizin...
The NASTRAN model plan for the fairing structure was expanded in detail to generate the NASTRAN mode...
The development of a structural finite element model for a generic transonic transport is presented....
Numerical results from a finite element analysis of rotodomed aircraft are presented. Automatic Mult...
Static Analysis of Rotodomed Aircra.t teas, been carries out usi Automatic Multistage Substructure (...
Stress analysis of an assemblage of HS-748 fuselage,\ud pylons and platform is carried out employing...
pCRM9 aeroelastic aircraft wing model for NASTRAN without RBE2 Based on the model published by Paul...
The use of NASTRAN at Bell Helicopter Company for structural static and dynamic analysis of a helico...
An application of NASTRAN to the structural analysis of light aircraft was conducted to determine th...
Stress analysis of metallic rudder of MiG-21 is carried out by finite element technique using the so...
This report contains the details of finite element analysis of radome for Mirage 2000. The radome is...
The objective of static testing of metallic rudder was to determine its sparline and trailing edge d...
The mathematical models and data used in the off-line flight simulation of the rotodomed aircraft ha...
The fuselage is an airplane’s main body section that holds crew and passengers. The design of a fuse...
The development of new air- and rotorcraft is very challenging. The design process is divided into t...
This paper introduces a fully parameterized finite element based tool chain for the structural sizin...
The NASTRAN model plan for the fairing structure was expanded in detail to generate the NASTRAN mode...
The development of a structural finite element model for a generic transonic transport is presented....