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Synonyms were used for: Conference • Dynamics • Materials • Structural Dynamics
Search without synonyms: title: 31st Structures, Structural Dynamics and Materials Conference

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Wind tunnel investigation of active controls technology applied to a DC-10 derivative

Winther, B. A. / Shirley, W. A. / Heimbaugh, R. M. | NTRS | 1980

efficiency and structural weight. As part of the NASA Energy Efficient Transport program, the impact upon flutter and gust load characteristics has ...

Publisher: NASA National Aeronautics and Space Administration

Keywords: Aircraft Stability And Control

Wind-tunnel evaluation of NASA developed control laws for flutter suppression on a DC-10 derivative wing

Abel, I. / Newsom, J. R. | NTRS | 1981

Two flutter suppression control laws have been synthesized, implemented, and tested on a low-speed aeroelastic wing model of a DC-10 ...

Publisher: NASA National Aeronautics and Space Administration

Keywords: Aircraft Design, Testing And Performance

Validation of a Flexible Aircraft TakeOff and Landing Analysis /FATOLA/ computer program using flight landing data

Carden, H. D. / Mcgehee, J. R. | NTRS | 1977

A multiple-degree-of-freedom takeoff and landing analysis, Flexible Aircraft TakeOff and Landing Analysis computer program (FATOLA), was ...

Publisher: NASA National Aeronautics and Space Administration

Keywords: Aircraft Design, Testing And Performance

Transonic flutter study of a wind-tunnel model of a supercritical wing with/without winglet

Ruhlin, C. L. / Rauch, F. J., Jr. / Waters, C. | NTRS | 1982

. The model was tested cantilever-mounted with a normal wingtip, a wingtip with winglet, and a normal wingtip ballasted to simulate the winglet ...

Publisher: NASA National Aeronautics and Space Administration

Keywords: Structural Mechanics

Transonic flutter study of a wind-tunnel model of an arrow-wing supersonic transport

Ruhlin, C. L. / Pratt-Barlow, C. R. | NTRS | 1981

changed the flutter mode from symmetric to antisymmetric. Vibration and flutter analyses were made using a finite-element structural ...

Publisher: NASA National Aeronautics and Space Administration

Keywords: Structural Mechanics

Transonic flutter and gust-response tests and analyses of a wind-tunnel model of a torsion-free-wing fighter airplane

Ruhlin, C. L. / Murphy, A. C. | NTRS | 1981

The paper reports the results of analytical and exploratory wind-tunnel studies of the transonic flutter and gust response characteristics ...

Publisher: NASA National Aeronautics and Space Administration

Keywords: Structural Mechanics

The European Spacelab structural design evolution

Thirkettle, A. J. | NTRS | 1982

low earth orbit in the cargo bay of the Shuttle Transportation System (STS) Orbiter. A description is presented of the structural development ...

Publisher: NASA National Aeronautics and Space Administration

Keywords: Spacecraft Design, Testing And Performance

Synthesis of structural damping.

Bieber, R. E. / Chang, C. S. | NTRS | 1968

Keywords: Structural Mechanics

Surface-pressure fluctuations associated with aerodynamic noise on the space shuttle launch configuration at transonic and supersonic speeds

Hanly, R. D. | NTRS | 1976

phase of the full-scale vehicle. A 120-channel data acquisition and reduction system was employed to obtain fluctuating pressure measurements ...

Publisher: NASA National Aeronautics and Space Administration

Structural synthesis of integrally stiffened cylinders.

Kicher, T. P. | NTRS | 1968

Structural design of stiffened cylindrical shells, discussing minimum weight, prevention of buckling modes, etc ...

Publisher: JOURNAL OF SPACECRAFT AND ROCKETS, VOL. 5, P. 62-67.

Keywords: Structural Mechanics