Improved flight test procedures for flutter clearance

Taxiing, take-off, and landing simulation of the high speed civil transport aircraft

Quasi-static and dynamic response characteristics of F-4 bias-ply and radial-belted main gear tires

Implementation of free-formulation-based flat shell elements into NASA comet code and development of nonlinear shallow shell element

Detection of non-symmetrical damage in smart plate-like structures

CM-2 environmental/modal testing of Spacehab racks

Coupled fluid-structure model for improved evaluation of vestibular function during in-flight conditions

The role of structural dynamics in the design and operations of space systems

Measurements of unsteady pressure and structural response for an elastic supercritical wing

Reciprocity-based experimental determination of dynamic forces and moments

Modeling the effect of shroud contact and friction dampers on the mistuned response of turbopumps

Dynamic response of NASA rotor test apparatus and Sikorsky S-76 hub mounted in the 80- by 120-foot wind tunnel

Application of the spectral element method to acoustic radiation

The structural dynamics analysis of the main injector LOX inlet tee and its redesign

Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack

F-15B/flight test fixture II

Performance analysis of two early NACA high speed propellers with application to civil tiltrotor configurations

Fuzzy logic decoupled lateral control for general aviation airplanes

Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments