This paper presents the results of recently-completed research and presents status reports of current research being performed within the Aeroelasticity Branch of the NASA Langley Research Center. Within the paper this research is classified as experimental, analytical, and theoretical aeroelastic research. The paper also describes the Langley Transonic Dynamics Tunnel, its features, capabilities, a new open-architecture data acquisition system, ongoing facility modifications, and the subsequent calibration of the facility
The Transonic Dynamics Tunnel (TDT) became in operational in 1960, and since that time has achieved ...
The application of active controls technology to reduce aeroelastic response of aircraft structures ...
"Prepared for Langley Research Center under Grant NGL 05-020-243."Bibliography: p. 146-154.Mode of a...
Historical Perspective on Aeroelasticity A LTHOUGH this paper is about the NASA Langley ResearchCent...
An overview of recently completed programs in aeroelasticity and structural dynamics research at the...
By the 1960s, researchers began to investigate the feasibility of using active controls technology (...
An overview of recently completed programs in aeroelasticity and structural dynamics research at the...
Testing of wind-tunnel aeroelastic models is a well established, widely used means of studying flutt...
The NASA Langley Aeroelasticity Branch is involved in a number of research programs related to fixed...
Recent progress in aeroelasticity, particularly at the NASA Langley Research Center is reviewed to l...
A status report is provided on the collaboration between the Royal Institute of Technology (KTH) in ...
This paper presents a status report on the collaboration between the Royal Institute of Technology (...
A historical account of the contributions of the Aeroelasticity Branch (AB) and the Langley Transoni...
Highlights of nine different research studies are described. Five of these topics relate directly to...
NASA conducts wind tunnel experiments to determine and understand the aeroelastic characteristics of...
The Transonic Dynamics Tunnel (TDT) became in operational in 1960, and since that time has achieved ...
The application of active controls technology to reduce aeroelastic response of aircraft structures ...
"Prepared for Langley Research Center under Grant NGL 05-020-243."Bibliography: p. 146-154.Mode of a...
Historical Perspective on Aeroelasticity A LTHOUGH this paper is about the NASA Langley ResearchCent...
An overview of recently completed programs in aeroelasticity and structural dynamics research at the...
By the 1960s, researchers began to investigate the feasibility of using active controls technology (...
An overview of recently completed programs in aeroelasticity and structural dynamics research at the...
Testing of wind-tunnel aeroelastic models is a well established, widely used means of studying flutt...
The NASA Langley Aeroelasticity Branch is involved in a number of research programs related to fixed...
Recent progress in aeroelasticity, particularly at the NASA Langley Research Center is reviewed to l...
A status report is provided on the collaboration between the Royal Institute of Technology (KTH) in ...
This paper presents a status report on the collaboration between the Royal Institute of Technology (...
A historical account of the contributions of the Aeroelasticity Branch (AB) and the Langley Transoni...
Highlights of nine different research studies are described. Five of these topics relate directly to...
NASA conducts wind tunnel experiments to determine and understand the aeroelastic characteristics of...
The Transonic Dynamics Tunnel (TDT) became in operational in 1960, and since that time has achieved ...
The application of active controls technology to reduce aeroelastic response of aircraft structures ...
"Prepared for Langley Research Center under Grant NGL 05-020-243."Bibliography: p. 146-154.Mode of a...