A technique for gust load alleviation (GLA) flight testing that will approximate a turbulence-like excitation of the wing has been devised. An artificial excitation is produced by randomly deflecting inboard control surfaces on the wing, thereby producing incremental loads on the wing. This presentation covers the background and development of the flight test technique and analyses performed to date
The design of the flutter suppression system for a remotely-piloted research vehicle is described. T...
A comprehensive gust response analysis was performed on a complete model of an airplane using the NA...
In response to the concerns of the aeroelastic community, NASA Dryden Flight Research Center, Edward...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
A brief review is presented of the basic methods of gust alleviation. Some results obtained in fligh...
Flight flutter-test results of the first aeroelastic research wing (ARW-1) of NASA's drones for aero...
The Subsonic Ultra Green Aircraft Research (SUGAR) Truss-Braced Wing (TBW) aeroservoelastic (ASE) wi...
This paper reviews the test techniques developed over the last several decades for flight flutter te...
A research excitation system was test flown at the NASA Dryden Flight Research Facility on the two-s...
Results are given of an analysis of wing and horizontal-tail spar strains measured on a twin-engine ...
An analytical study has shown that a gust alleviation system for a STOL airplane in a cruise conditi...
Douglas Aircraft Company experience in flight flutter testing is reviewed briefly, with comments on ...
A wind-tunnel technique which makes use of a dynamically scaled aeroelastic model to predict full-sc...
A software program and associated methodology to study gust loading on aircraft exists for a classif...
A study to develop analytical procedures to be used in the checkout and calibration of a flutter win...
The design of the flutter suppression system for a remotely-piloted research vehicle is described. T...
A comprehensive gust response analysis was performed on a complete model of an airplane using the NA...
In response to the concerns of the aeroelastic community, NASA Dryden Flight Research Center, Edward...
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a D...
A brief review is presented of the basic methods of gust alleviation. Some results obtained in fligh...
Flight flutter-test results of the first aeroelastic research wing (ARW-1) of NASA's drones for aero...
The Subsonic Ultra Green Aircraft Research (SUGAR) Truss-Braced Wing (TBW) aeroservoelastic (ASE) wi...
This paper reviews the test techniques developed over the last several decades for flight flutter te...
A research excitation system was test flown at the NASA Dryden Flight Research Facility on the two-s...
Results are given of an analysis of wing and horizontal-tail spar strains measured on a twin-engine ...
An analytical study has shown that a gust alleviation system for a STOL airplane in a cruise conditi...
Douglas Aircraft Company experience in flight flutter testing is reviewed briefly, with comments on ...
A wind-tunnel technique which makes use of a dynamically scaled aeroelastic model to predict full-sc...
A software program and associated methodology to study gust loading on aircraft exists for a classif...
A study to develop analytical procedures to be used in the checkout and calibration of a flutter win...
The design of the flutter suppression system for a remotely-piloted research vehicle is described. T...
A comprehensive gust response analysis was performed on a complete model of an airplane using the NA...
In response to the concerns of the aeroelastic community, NASA Dryden Flight Research Center, Edward...