Linear unsteady aerodynamic models are obtained for a NACA 0006 airfoil in a wind tunnel experiment at Reynolds number 65,000. A family of system identification maneuvers, based on a canonical step-up, hold maneuver, are specifically designed to extract relevant unsteady information from phase averaged wind tunnel measurements. Linear models based on these maneuvers are constructed using OKID/E...

This should be a good book for use in teachij^ higher school classes and junior science students t / main facts of human anatomy including microscop anatomy or histology. It is not recommended for } , medical student, however, because with the lirn't .g time available in the average medical course i' j necessary for him to plunge direct into a detau study of the subject without spending any tim...

In classical aeroelasticity, the typical at plate section consists of two degrees of freedom, namely pitch and plunge. Current resources o er the capability of enhancing the response of the typical aerofoil by making it adaptive. This project investigates the dynamic aeroelastic e ects of two of these options: trailing edge aps and chordwise (camber) deformations. The structural model is assume...

This paper presents the design of NetPIPE, a new Network Protocol Independent Performance Evaluator. NetPIPE maps the performance of a network across a wide range and presents the data in a new manner. Its protocol independence allows for visualization of the overhead associated with a protocol layer. Using Net-PIPE has led to the discovery of a deep plunge in ATM performance for certain transf...

Among the members of the Association of Southeast Asian Nations (ASEAN), there are wide economic gaps between more developed countries including Singapore and Thailand and less developed ones including Vietnam. The gaps represents one of the largest obstacles to realizing the ASEAN’s goal of market integration and the situation is at risk of getting even worse next year, as it is increasingly l...

Nomenclature C = chord length, m C T = thrust coefficient f = flapping frequency, Hz h tip = plunge amplitude at the wing tip, m k = ωC∕U ∞ , reduced frequency l span = wingspan, m Re = U ∞ C∕ν, Reynolds number r z = z-directional distance away from the wing tip, m S wing = wing area, m 2 St = fh tip ∕U ∞ , Strouhal number U ∞ = freestream velocity, m∕s ν = kinematic viscosity of fluid, m 2 ∕s ...

woman seeking relief from menopausal.svmptoms is common in Westesn society. Many women, however, suffer in silence or take the plunge towards synthetic hormone replacement therapy (HRT). Whilst the untoward symptoms of the female climacteric (change of life) are troublesome, the postmenopausal onslaught of degenerative diseases is the real health problem that faces the mature female. New inform...