Add to ORKGThis report gives the results of a detailed study of the flutter characteristics of four representative aircraft wings. This study was made using the electric-analog computer at the California Institute of Technology. During the course of this investigation eight important parameters of each wing were varied and, in addition, the effects of mass, inertia, pitching spring, and location of a concentrated mass were investigated for all four wings and at several sweepback angles
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transpor...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
Flutter is the phenomenon where the body will experience uncontrolled motions after reaching a certa...
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...
This report gives the results of a detailed study of the flutter characteristics of four representat...
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter ...
The prwnt report gives the resu-h%oj a dgtaikd study of the flutter charadmktim ~four reprawntu$ivea...
An experimental investigation was made of a preloaded spring-tab flutter model to determine the effe...
An interactive computer program was developed for wing flutter analysis in the conceptual design sta...
In this work, flutter behaviour of NACA 6409 is investigated using wind tunnel. The plunging and pit...
Wind-tunnel flutter investigations at Mach numbers up to 0.30 have been conducted on a 40 degree swe...
An interactive computer program was developed for wing flutter analysis in the conceptual design sta...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...
Presents the results of sixty-six experimental flutter tests made on two uniform, cantilever wing mo...
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transpor...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
Flutter is the phenomenon where the body will experience uncontrolled motions after reaching a certa...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
"This report presents a survey of previous theoretical and experimental investigations on wing flutt...
This report gives the results of a detailed study of the flutter characteristics of four representat...
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter ...
The prwnt report gives the resu-h%oj a dgtaikd study of the flutter charadmktim ~four reprawntu$ivea...
An experimental investigation was made of a preloaded spring-tab flutter model to determine the effe...
An interactive computer program was developed for wing flutter analysis in the conceptual design sta...
In this work, flutter behaviour of NACA 6409 is investigated using wind tunnel. The plunging and pit...
Wind-tunnel flutter investigations at Mach numbers up to 0.30 have been conducted on a 40 degree swe...
An interactive computer program was developed for wing flutter analysis in the conceptual design sta...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...
Presents the results of sixty-six experimental flutter tests made on two uniform, cantilever wing mo...
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transpor...
A review is presented of the work done by other investigators on the effects of inertia couplings in...
Flutter is the phenomenon where the body will experience uncontrolled motions after reaching a certa...