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
Small aircraft manufacturers are typically constrained by stringent budget requirements. Among all t...
An analysis of the flight time-history records of a record-propelled 60 degree delta-wing airplane c...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter ...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
"This report presents a survey of previous theoretical and experimental investigations on wing flutt...
Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. ...
Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
Wind-tunnel flutter investigations at Mach numbers up to 0.30 have been conducted on a 40 degree swe...
A summary is presented of experiences in connection with flight flutter testing of supersonic interc...
Flutter may be considered to be one of the most dangerous aeroelastic failure phenomenon. The flutt...
Small aircraft manufacturers are typically constrained by stringent budget requirements. Among all t...
An analysis of the flight time-history records of a record-propelled 60 degree delta-wing airplane c...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter ...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
"This report presents a survey of previous theoretical and experimental investigations on wing flutt...
Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. ...
Wind tunnel investigation of transonic and supersonic flutter of air to surface missile vertical tai...
Several very low aspect ratio flat plate wing configurations are analyzed for their aerodynamic inst...
Wind-tunnel flutter investigations at Mach numbers up to 0.30 have been conducted on a 40 degree swe...
A summary is presented of experiences in connection with flight flutter testing of supersonic interc...
Flutter may be considered to be one of the most dangerous aeroelastic failure phenomenon. The flutt...
Small aircraft manufacturers are typically constrained by stringent budget requirements. Among all t...
An analysis of the flight time-history records of a record-propelled 60 degree delta-wing airplane c...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...