Cylindrical ShellOptimization of Composite Stiffened Cylindrical Shell using PSO Algorithm [Volume 11, Issue 2, 2017, Pages 43-51]
D
Donnel theoryA Parametric Study for Vibration Analysis of Composite Cylindrical Shell Resting under Elastic Foundation: Analytical and Numerical Methods [Volume 11, Issue 2, 2017, Pages 13-22]
E
Exact SolutionBuckling and Post-buckling Analysis of FG-CNTRC Beams: An Exact Closed Form Solution [Volume 11, Issue 2, 2017, Pages 33-41]
F
Fatigue lifeFatigue Life Assessment of Composite Airplane Wing Subjected to Variable Mechanical and Thermal Loads [Volume 11, Issue 2, 2017, Pages 1-11]
Finite ElementLoading Estimation of Flapping Wings under Aeroelastic Effect Using Finite Element Method [Volume 11, Issue 1, 2017]
Finite ElementA Parametric Study for Vibration Analysis of Composite Cylindrical Shell Resting under Elastic Foundation: Analytical and Numerical Methods [Volume 11, Issue 2, 2017, Pages 13-22]
Finite element methodLocal Imperfection Effects on Thermal Buckling Behavior of Composite Fiber Reinforced Truncated Conical Liner [Volume 11, Issue 1, 2017]
Finite element methodFatigue Life Assessment of Composite Airplane Wing Subjected to Variable Mechanical and Thermal Loads [Volume 11, Issue 2, 2017, Pages 1-11]
Flapping wingLoading Estimation of Flapping Wings under Aeroelastic Effect Using Finite Element Method [Volume 11, Issue 1, 2017]
Local imperfectionLocal Imperfection Effects on Thermal Buckling Behavior of Composite Fiber Reinforced Truncated Conical Liner [Volume 11, Issue 1, 2017]
M
Mechanical and thermal loadsFatigue Life Assessment of Composite Airplane Wing Subjected to Variable Mechanical and Thermal Loads [Volume 11, Issue 2, 2017, Pages 1-11]
N
Nano-composite beamsBuckling and Post-buckling Analysis of FG-CNTRC Beams: An Exact Closed Form Solution [Volume 11, Issue 2, 2017, Pages 33-41]
Nero adaptive controlAdaptive Quaternion Attitude Control of Aerodynamic Flight Control Vehicles [Volume 11, Issue 2, 2017, Pages 23-32]
P
Post-buckling analysisBuckling and Post-buckling Analysis of FG-CNTRC Beams: An Exact Closed Form Solution [Volume 11, Issue 2, 2017, Pages 33-41]
PSO algorithmOptimization of Composite Stiffened Cylindrical Shell using PSO Algorithm [Volume 11, Issue 2, 2017, Pages 43-51]
Pulse-Width Pulse-Frequency ModulatorPreliminary Design of Spacecraft Attitude Control with Pulse-Width Pulse-Frequency Modulator for Rest-to-Rest Maneuvers [Volume 11, Issue 1, 2017]
Q
Quasi-NormalizationPreliminary Design of Spacecraft Attitude Control with Pulse-Width Pulse-Frequency Modulator for Rest-to-Rest Maneuvers [Volume 11, Issue 1, 2017]
Quaternion attitude controlAdaptive Quaternion Attitude Control of Aerodynamic Flight Control Vehicles [Volume 11, Issue 2, 2017, Pages 23-32]
Spacecraft attitude controlPreliminary Design of Spacecraft Attitude Control with Pulse-Width Pulse-Frequency Modulator for Rest-to-Rest Maneuvers [Volume 11, Issue 1, 2017]
T
Thermal bucklingLocal Imperfection Effects on Thermal Buckling Behavior of Composite Fiber Reinforced Truncated Conical Liner [Volume 11, Issue 1, 2017]
Transmission LossOptimization of Sound Transmission Loss of a Composite Rectangular Plate with Infinite Baffle [Volume 11, Issue 2, 2017, Pages 53-63]