Results 111 to 120 of about 135,451 (244)

Experimental Classical Flutter Reesults of a Composite Advanced Turboprop Model [PDF]

open access: yes
Experimental results are presented that show the effects of blade pitch angle and number of blades on classical flutter of a composite advanced turboprop (propfan) model.
Kaza, K. R. V., Mehmed, O.
core   +1 more source

Wind tunnel investigation of supersonic wing-tail flutter [PDF]

open access: yes
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was tested in a 4-foot transonic tunnel in the Mach number range 1.1 to 1.3.
Holsapple, D. E.   +2 more
core   +1 more source

Pseudoventricular Flutter [PDF]

open access: yesBaylor University Medical Center Proceedings, 2007
D Luke, Glancy   +3 more
openaire   +2 more sources

Comparison of analytical and wind-tunnel results for flutter and gust response of a transport wing with active controls [PDF]

open access: yes
Two flutter suppression control laws wre designed and tested on a low speed aeroelastic model of a DC-10 derivative wing. Both control laws demontrated increases in flutter speed in excess of 25 percent above the passive wing flutter speed.
Abel, I., Newsom, J. R., Perry, B., III
core   +1 more source

Flutter of panels on discrete flexible supports [PDF]

open access: yes
The supersonic flutter of wide panels on discrete flexible supports is investigated for three different panel-support configurations. The first study examines the effect of support stiffness on the flutter behavior of a specific five-support ...
Stein, M.
core   +1 more source

Flutter Prediction for Aircraft Conceptual Design [PDF]

open access: yes
Flutter prediction is usually a knowledge-based analysis process that aims to reduce the cost of aeroelastic stability margin certification. However, early detection of flutter problems is beneficial in the development of unconventional aircraft.
Geiselhart, Karl, Li, Wu, Robinson, Jay
core   +1 more source

A theory of flight flutter testing [PDF]

open access: yes
Flight flutter testing is considered as a method for finding generalized aerodynamic forces. The coefficients determined from flight flutter tests are used in flutter calculations, using a simple expansion in frequency and Mach number.
Molloe-Christensen, E.
core   +1 more source

Home - About - Disclaimer - Privacy