Presented is a limited review of some experiences in flight testing of missiles and of wing flutter investigations that may be of interest in missile design. Several types of flutter of concern in missile studies are briefly described. Crude criteria are presented for two of the most common types of flutter to permit a rapid estimate to be made of the probability of the occurrence of flutter. Many of the details of the flutter problem have been omitted, and only the broader elements have been retained so as to give the designer an overall view of the subject
For light aircraft, especially gliders, it is too expensive to apply the same extensive flutter anal...
An empirical method is specified which can be used by the manufacturers of gliders and small aircraf...
For light aircraft, especially gliders, it is too expensive to apply the same extensive flutter anal...
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter ...
A summary is presented of experiences in connection with flight flutter testing of supersonic interc...
The design of a cruise missile wing is a multidisciplinary work, since the wing has to provide enoug...
"The paper outlines the theoretical and experimental procedure one has to adopt for flutter prevent...
Flutter may be considered to be one of the most dangerous aeroelastic failure phenomenon. The flutt...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
Flutter is a catastrophic aeroelastic instability that must be prevented for all engineering structu...
Purpose - This paper sets out to provide a general review of the flight flutter test techniques util...
One of the most dangerous aeroelastic failure phenomenon is flutter. The flutter characteristic is d...
The technical memorandum briefly summarizes the growth of interest in aeroelastic phenomena as aircr...
Small aircraft manufacturers are typically constrained by stringent budget requirements. Among all t...
For light aircraft, especially gliders, it is too expensive to apply the same extensive flutter anal...
An empirical method is specified which can be used by the manufacturers of gliders and small aircraf...
For light aircraft, especially gliders, it is too expensive to apply the same extensive flutter anal...
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter ...
A summary is presented of experiences in connection with flight flutter testing of supersonic interc...
The design of a cruise missile wing is a multidisciplinary work, since the wing has to provide enoug...
"The paper outlines the theoretical and experimental procedure one has to adopt for flutter prevent...
Flutter may be considered to be one of the most dangerous aeroelastic failure phenomenon. The flutt...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
Flutter is a catastrophic aeroelastic instability that must be prevented for all engineering structu...
Purpose - This paper sets out to provide a general review of the flight flutter test techniques util...
One of the most dangerous aeroelastic failure phenomenon is flutter. The flutter characteristic is d...
The technical memorandum briefly summarizes the growth of interest in aeroelastic phenomena as aircr...
Small aircraft manufacturers are typically constrained by stringent budget requirements. Among all t...
For light aircraft, especially gliders, it is too expensive to apply the same extensive flutter anal...
An empirical method is specified which can be used by the manufacturers of gliders and small aircraf...
For light aircraft, especially gliders, it is too expensive to apply the same extensive flutter anal...