The prwnt report gives the resu-h%oj a dgtaikd study of the flutter charadmktim ~four reprawntu$iveaircrajlm“ngs. Thti study was md using the ele~”a-ana.tog computer at the Cali-fornia Imtitut.e of Technology. During the cour8e of thti investigation ~“ght importunt paramet.em of each mung were varied and, in addition, the e$ea % of mass, inertia, pitching Spn”ng,and location of a CO?W8?UW&?d7nu88were inv~”gai.ed for alljour m“ngsand al severalsweepbackangles. The introduction of thiareport discuss ~ in general ternMtti jluti characteristics of airp.kuw. The second section con-tain8 a A.ww-ssionof the electric-analogprincipl ~ thd made a study of thi8 magnitti fem”ble. The third section contuirwa discussion of the amodynamic and structur...
ABSTRACT: The dynamic and aeroelastic characteristic of a transport aircraft has been established us...
In this paper, the relevance of propeller whirl flutter for (hybrid-) electric aircraft configuratio...
An interactive computer program was developed for wing flutter analysis in the conceptual design sta...
This report gives the results of a detailed study of the flutter characteristics of four representat...
This report gives the results of a detailed study of the flutter characteristics of four representat...
Part I describes vibration tests, in a wind tunnel, of simple airfoils and of the tail plane of an M...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
AbstractEvery object has its own natural frequency when the frequency of a source is equal to the ob...
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1947Bib...
"The paper outlines the theoretical and experimental procedure one has to adopt for flutter prevent...
Flutter is a catastrophic aeroelastic instability that must be prevented for all engineering structu...
One of many problems in the field of sailplane design is that of aeroelastic stability. Practicing ...
Presents the results of sixty-six experimental flutter tests made on two uniform, cantilever wing mo...
EU Operational Programme Research, Development and Education, and from the Center of Advanced Aerosp...
A summary is presented of experiences in connection with flight flutter testing of supersonic interc...
ABSTRACT: The dynamic and aeroelastic characteristic of a transport aircraft has been established us...
In this paper, the relevance of propeller whirl flutter for (hybrid-) electric aircraft configuratio...
An interactive computer program was developed for wing flutter analysis in the conceptual design sta...
This report gives the results of a detailed study of the flutter characteristics of four representat...
This report gives the results of a detailed study of the flutter characteristics of four representat...
Part I describes vibration tests, in a wind tunnel, of simple airfoils and of the tail plane of an M...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
AbstractEvery object has its own natural frequency when the frequency of a source is equal to the ob...
Thesis: M.S., Massachusetts Institute of Technology, Department of Aeronautical Engineering, 1947Bib...
"The paper outlines the theoretical and experimental procedure one has to adopt for flutter prevent...
Flutter is a catastrophic aeroelastic instability that must be prevented for all engineering structu...
One of many problems in the field of sailplane design is that of aeroelastic stability. Practicing ...
Presents the results of sixty-six experimental flutter tests made on two uniform, cantilever wing mo...
EU Operational Programme Research, Development and Education, and from the Center of Advanced Aerosp...
A summary is presented of experiences in connection with flight flutter testing of supersonic interc...
ABSTRACT: The dynamic and aeroelastic characteristic of a transport aircraft has been established us...
In this paper, the relevance of propeller whirl flutter for (hybrid-) electric aircraft configuratio...
An interactive computer program was developed for wing flutter analysis in the conceptual design sta...