23 research outputs found
Flutter Investigation in the Transonic Range of Six Airfoils Attached to Three Freely Falling Bodies
Get PDFSome experiments on the flutter of wings with sweepback in the transonic speed range utilizing rocket-propelled vehicles
Get PDFFlutter of a 60 degree delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model
Get PDFFlutter Investigation in the High Subsonic and Transonic Speed Range on Cantilever Delta-wing Plan Forms with Leading-edge Sweepback of 60 Degrees, 53 Degrees 8', and 45 Degrees
Get PDFSupersonic flutter of a 60 degree delta wing encountered during the flight test of a rocket-propelled model
Get PDFResults of two free-fall experiments on flutter of thin unswept wings in the transonic speed range
Get PDFNote on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model
Get PDFResults of Two Free-fall Experiments on Flutter of Thin Unswept Wings in the Transonic Speed Range
Get PDFResults of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. Two airfoils fluttered at a Mach number of 0.85, a third airfoil fluttered at a Mach number of 1.03, and a fourth fluttered at a Mach number of 1.07. Results of calculations of flutter speed using incompressible and compressible air-force coefficients, including a Mach number of 1.0, are presented
Investigation of an All-moveable Control Surface at a Mach Number of 6.86 for Possible Flutter
Get PDFFree-flight Tests of 45 Degree Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds
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