Results 111 to 120 of about 21,307 (261)

Progress in aeroelastic optimization - Analytical versus numerical approaches [PDF]

open access: yes
Mathematical and structural analysis for optimal control of aeroelasticity in unswept ...
Ashley, H.   +2 more
core   +1 more source

A Time-Domain Calculation Method for Gust Aerodynamics in Flight Simulation

open access: yesAerospace
Gusts have a significant impact on aircraft and need to be analyzed through flight simulations. The solution for time-domain gust aerodynamic forces stands as a pivotal stage in this process. With the increasing demand for flight simulations within gusty
Zexuan Yang   +4 more
doaj   +1 more source

Structural dynamics branch research and accomplishments for fiscal year 1987 [PDF]

open access: yes
This publication contains a collection of fiscal year 1987 research highlights from the Structural Dynamics Branch at NASA Lewis Research Center. Highlights from the branch's four major work areas, Aeroelasticity, Vibration Control, Dynamic Systems, and ...

core   +1 more source

Computational engine structural analysis [PDF]

open access: yes
A significant research activity at the NASA Lewis Research Center is the computational simulation of complex multidisciplinary engine structural problems.
Chamis, C. C., Johns, R. H.
core   +1 more source

Numerical and Experimental Study of Flutter in a Realistic Labyrinth Seal

open access: yesInternational Journal of Turbomachinery, Propulsion and Power
Labyrinth seals are commonly used in turbomachinery in order to control leakage flows. Flutter is one of the most dangerous potential issues for them, leading to High Cycle Fatigue (HCF) life considerations or even mechanical failure.
Oscar Bermejo   +5 more
doaj   +1 more source

Design and analysis issues of integrated control systems for high-speed civil transports [PDF]

open access: yes
A study was conducted to identify, rank, and define development plans for the critical guidance and control design and analysis issues as related to economically viable and environmentally acceptable high-speed civil transport. The issues were identified
Dykman, John R.   +4 more
core   +1 more source

Identification of unsteady aerodynamics and aeroelastic integro-differential systems [PDF]

open access: yes
The problem of estimating integro-differential models based on test or simulation data is dealt with. The identification techniques proposed for estimating parameters in models described by differential equations need to be considerably extended to deal ...
Gupta, N. K., Iliff, K. W.
core   +1 more source

Prediction of transonic flutter for a supercritical wing by modified strip analysis and comparison with experiment [PDF]

open access: yes
Use of a supercritical airfoil can adversely affect wing flutter speeds in the transonic range. As adequate theories for three dimensional unsteady transonic flow are not yet available, the modified strip analysis was used to predict the transonic ...
Desmarais, R. N.   +3 more
core   +1 more source

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