It has long been recognized that frequency and phasing of structural modes in the presence of airflow play a fundamental role in the occurrence of flutter. Animation of simulation results for the long, slender Semi-Span Super-Sonic Transport (S4T) wind-tunnel model demonstrates that, for the case of mass-ballasted nacelles, the flutter mode can be described as a traveling wave propagating downstream. Such a characterization provides certain insights, such as (1) describing the means by which energy is transferred from the airflow to the structure, (2) identifying airspeed as an upper limit for speed of wave propagation, (3) providing an interpretation for a companion mode that coalesces in frequency with the flutter mode but becomes very we...
As part of a morphing wing technology project, the flutter analysis of two finite element models and...
A time-marching aeroelastic method developed for the study of propeller flutter is presented and val...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
A study to develop analytical procedures to be used in the checkout and calibration of a flutter win...
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transpor...
A summary of computational and experimental aeroelastic and aeroservoelastic (ASE) results for the S...
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was t...
A virtual wind tunnel is developed by combin-ing a fast, time-stepping ow solver with an interac-ti...
The stability boundaries of a very flexible wing are sought to inform a wind-tunnel flutter test cam...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
This paper presents high fidelity Navier-Stokes simulations of the Boeing Subsonic Ultra Green Aircr...
Supersonic flows cause thin panels to flutter, which is characterized by high-amplitude self-sustain...
In this work, flutter behaviour of NACA 6409 is investigated using wind tunnel. The plunging and pit...
As part of a morphing wing technology project, the flutter analysis of two finite element models and...
A time-marching aeroelastic method developed for the study of propeller flutter is presented and val...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
A study to develop analytical procedures to be used in the checkout and calibration of a flutter win...
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transpor...
A summary of computational and experimental aeroelastic and aeroservoelastic (ASE) results for the S...
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was t...
A virtual wind tunnel is developed by combin-ing a fast, time-stepping ow solver with an interac-ti...
The stability boundaries of a very flexible wing are sought to inform a wind-tunnel flutter test cam...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
This paper describes the development of a new state-of-the-art large wind tunnel model for active fl...
This paper presents high fidelity Navier-Stokes simulations of the Boeing Subsonic Ultra Green Aircr...
Supersonic flows cause thin panels to flutter, which is characterized by high-amplitude self-sustain...
In this work, flutter behaviour of NACA 6409 is investigated using wind tunnel. The plunging and pit...
As part of a morphing wing technology project, the flutter analysis of two finite element models and...
A time-marching aeroelastic method developed for the study of propeller flutter is presented and val...
Two flutter suppression control laws were synthesized, implemented, and tested on a low speed aeroel...