Flutter analysis of composite wings using an exact dynamic stiffness matrix method
Flutter Analysis of Composite Wings Using an Exact Dynamic Stiffness Matrix Method
Optimum design of high aspect ratio wings subject to aeroelastic constraints
Optimum Design of High Aspect Ratio Wings Subject to Aeroelastic Constraints
A Study of Rockets as Passive Controllers
Gust Alleviation and Flutter Suppression of an Optimized Composite Wing with Active Control
Reference systems for laser beam quality and parameter measurements [2889-546]
Deep-etched multiphase level fractional Talbot grating [2885-560]
Efficient method for resisting humidity into MBDCG holograms [2885-536]
Prelase A-O mode-locked Cr:LiSAF laser pumped by flashlamp [2889-596]
Generation of 3D image from computer data with dot array rainbow hologram (Invited Paper) [2885-524]
Electro-optic modulator with quasi-velocity matching [2997-27]
Method for improving performance of IR focal plane array using microlens array [3099-12]
Reliability predictions on fiber gratings through alternate methods
Investigation on environmental stability of DCG holograms by molecule enclosure [3011-42]
Fuel/Propellant Mixing in an Open-Cycle Gas Core Nuclear Rocket Engine
Study of the electro-optic polymer films with improved properties
Q-switching of 10W fiber coupled diode laser pumped Nd:YAG