Add to ORKGSubsonic and supersonic flutter calculations on swept and unswept wings to evaluate effects of variations in aerodynamic parameters and densit
Design for prevention of aeroelastic instability (that is, the critical speeds leading to aeroelasti...
This report gives the results of a detailed study of the flutter characteristics of four representat...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...
An investigation of the flutter characteristics of a series of thin cantilever wings having taper ra...
"January 1960."Cover title.Includes bibliographical references (p. 22-23).Mode of access: Internet
Presents the results of sixty-six experimental flutter tests made on two uniform, cantilever wing mo...
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was t...
The results of some wind-tunnel experiments to investigate the effects of aspect ratio and Mach numb...
Flutter characteristics of a cantilevered high aspect ratio wing with winglet were investigated. The...
Present flutter analysis methods do not accurately predict the flutter speeds in the transonic flow ...
The effects on flutter of the aerodynamic interaction between the space shuttle bodies and wing, 1/8...
An experimental and analytical study was conducted at Mach 0.7 to investigate the effects of spanwis...
Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. ...
Use of a supercritical airfoil can adversely affect wing flutter speeds in the transonic range. As a...
A 1/20-size, low-speed flutter model of the SCAT-15F complete airplane was tested on cables to simul...
Design for prevention of aeroelastic instability (that is, the critical speeds leading to aeroelasti...
This report gives the results of a detailed study of the flutter characteristics of four representat...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...
An investigation of the flutter characteristics of a series of thin cantilever wings having taper ra...
"January 1960."Cover title.Includes bibliographical references (p. 22-23).Mode of access: Internet
Presents the results of sixty-six experimental flutter tests made on two uniform, cantilever wing mo...
A flutter model, consisting of a wing, horizontal tail, and splitter plate/fuselage mechanism, was t...
The results of some wind-tunnel experiments to investigate the effects of aspect ratio and Mach numb...
Flutter characteristics of a cantilevered high aspect ratio wing with winglet were investigated. The...
Present flutter analysis methods do not accurately predict the flutter speeds in the transonic flow ...
The effects on flutter of the aerodynamic interaction between the space shuttle bodies and wing, 1/8...
An experimental and analytical study was conducted at Mach 0.7 to investigate the effects of spanwis...
Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. ...
Use of a supercritical airfoil can adversely affect wing flutter speeds in the transonic range. As a...
A 1/20-size, low-speed flutter model of the SCAT-15F complete airplane was tested on cables to simul...
Design for prevention of aeroelastic instability (that is, the critical speeds leading to aeroelasti...
This report gives the results of a detailed study of the flutter characteristics of four representat...
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers betwe...