Aircraft aeroelasticity and structural dynamics research at the NASA Langley Research Center: Some illustrative results [PDF]
Highlights of nine different research studies are described. Five of these topics relate directly to fixed-wing aircraft and range from flutter studies using relatively simple and inexpensive wind-tunnel models to buffet studies of the vertical tails of ...
Cazier, F. W., Jr. +1 more
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Response studies of rotors and rotor blades with application to aeroelastic tailoring [PDF]
Various tools for the aeroelastic stability and response analysis of rotor blades in hover and forward flight were developed and incorporated in a comprehensive package capable of performing aeroelastic tailoring of rotor blades in forward flight.
Friedmann, P. P.
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VIBRATIONS OF THIN WINGS IN THE SEPARATED FLOW. CALCULATION AND EXPERIMENT
Научный вестник МГТУ ГА, 2016 The results of computational and experimental study of thin wings flutter in separated and unseparated flow are presented. The effect of flutter suppressing in the presence of separation is found.
V. V. Ovchinnikov, Yu. V. Petrov
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Dataset of numerical simulations for aeroelastic control of an aero engine compressor cascade using plasma actuators. [PDF]
Data Brief, 2021 De Giorgi MG +3 more
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Effects of nonlinear aerodynamics and static aeroelasticity on mission performance calculations for a fighter aircraft [PDF]
During conceptual design studies of advanced aircraft, the usual practice is to use linear theory to calculate the aerodynamic characteristics of candidate rigid (nonflexible) geometric external shapes.
Foss, Willard E., Jr. +2 more
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Numerical and Experimental Study of Flutter in a Realistic Labyrinth Seal
International Journal of Turbomachinery, Propulsion and PowerLabyrinth 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
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NASA Lewis Research Center/University Graduate Research Program on Engine Structures [PDF]
NASA Lewis Research Center established a graduate research program in support of the Engine Structures Research activities. This graduate research program focuses mainly on structural and dynamics analyses, computational mechanics, mechanics of ...
Chamis, C. C.
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Reduced Order Modeling for Transonic Aeroservoelastic Control Law Development [PDF]
As aircraft become more flexible, aeroelastic considerations become increasingly important and complex, particularly for transonic flight where nonlinearities in the flow render linear analysis tools less effective.
Bartels, Robert E. +3 more
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Structural dynamics branch research and accomplishments for fiscal year 1987 [PDF]
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 ...
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Experimental and Numerical Investigation of Post-Flutter Limit Cycle Oscillations on a Cantilevered Flat Plate [PDF]
, 2017 Futuristic aircraft designs and novel aircraft such as High Altitude Long Endurance (HALE) involve a higher level of structural flexibility than in conventional aircraft.
Antonio Bernardo, Guimaraes Neto +5 more
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