In response to the concerns of the aeroelastic community, NASA Dryden Flight Research Center, Edwards, California, is conducting research into improving the flight flutter (including aeroservoelasticity) test process with more accurate and automated techniques for stability boundary prediction. The important elements of this effort so far include the following: (1) excitation mechanisms for enhanced vibration data to reduce uncertainty levels in stability estimates; (2) investigation of a variety of frequency, time, and wavelet analysis techniques for signal processing, stability estimation, and nonlinear identification; and (3) robust flutter boundary prediction to substantially reduce the test matrix for flutter clearance. These are criti...
Flight flutter testing is a mandatory test performed to demonstrate that prototype aircraft are free...
Modern aircraft employ a significant fraction of their weight in composite materials to reduce weigh...
The Skyrocket II is an all composite constructed experimental prototype airplane. A flutter clearanc...
Flight flutter testing is an integral part of flight envelope clearance. This paper discusses advanc...
Flight flutter-test results of the first aeroelastic research wing (ARW-1) of NASA's drones for aero...
Developments in methodology and data analysis techniques for flutter testing in flight and on the gr...
This paper reviews the test techniques developed over the last several decades for flight flutter te...
The goal of this program was to combine modern control concepts with new identification techniques t...
This paper documents an invited presentation given to The Boeing Company, Seattle, Washington, on Se...
Many parameter identification techniques have been used at the NASA Ames Research Center, Dryden Res...
Douglas Aircraft Company experience in flight flutter testing is reviewed briefly, with comments on ...
Papers presented at the conference are reported. Subjects discussed include: theory, methods and tec...
A summary is presented of experiences in connection with flight flutter testing of supersonic interc...
Wavelets present a method for signal processing that may be useful for analyzing responses of dynami...
Flutter of an aeroelastic structure is potentially destructive aeroelastic instability. This phenome...
Flight flutter testing is a mandatory test performed to demonstrate that prototype aircraft are free...
Modern aircraft employ a significant fraction of their weight in composite materials to reduce weigh...
The Skyrocket II is an all composite constructed experimental prototype airplane. A flutter clearanc...
Flight flutter testing is an integral part of flight envelope clearance. This paper discusses advanc...
Flight flutter-test results of the first aeroelastic research wing (ARW-1) of NASA's drones for aero...
Developments in methodology and data analysis techniques for flutter testing in flight and on the gr...
This paper reviews the test techniques developed over the last several decades for flight flutter te...
The goal of this program was to combine modern control concepts with new identification techniques t...
This paper documents an invited presentation given to The Boeing Company, Seattle, Washington, on Se...
Many parameter identification techniques have been used at the NASA Ames Research Center, Dryden Res...
Douglas Aircraft Company experience in flight flutter testing is reviewed briefly, with comments on ...
Papers presented at the conference are reported. Subjects discussed include: theory, methods and tec...
A summary is presented of experiences in connection with flight flutter testing of supersonic interc...
Wavelets present a method for signal processing that may be useful for analyzing responses of dynami...
Flutter of an aeroelastic structure is potentially destructive aeroelastic instability. This phenome...
Flight flutter testing is a mandatory test performed to demonstrate that prototype aircraft are free...
Modern aircraft employ a significant fraction of their weight in composite materials to reduce weigh...
The Skyrocket II is an all composite constructed experimental prototype airplane. A flutter clearanc...