Add to ORKGResults 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
NACA Research Memorandum L54D12A."September 25, 1952."Includes bibliographical references (p. 6).Mod...
Wind-tunnel flutter investigations at Mach numbers up to 0.30 have been conducted on a 40 degree swe...
A solution procedure was developed to investigate the two-dimensional, one- or two-dimensional flutt...
Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. ...
Flutter data in the transonic speed range for four nearly identical, thin, unswept wings have been o...
Two low-acceleration transonic-flutter vehicles were launched and flown. The first carried two test ...
"This report presents a survey of previous theoretical and experimental investigations on wing flutt...
Presents the results of sixty-six experimental flutter tests made on two uniform, cantilever wing mo...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
Results of flutter tests on some simple all-movable-control-type models are given. One set on models...
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter ...
"This report covers tests of a 5-foot model of the NACA 66,2-420 low-drag airfoil at high speeds inc...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The flutter of a pitch-and-plunge airfoil (PAPA) in transonic flow is simulated using two shock-capt...
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transpor...
NACA Research Memorandum L54D12A."September 25, 1952."Includes bibliographical references (p. 6).Mod...
Wind-tunnel flutter investigations at Mach numbers up to 0.30 have been conducted on a 40 degree swe...
A solution procedure was developed to investigate the two-dimensional, one- or two-dimensional flutt...
Results of four thin, unswept, flutter airfoils attached to two freely falling bodies are reported. ...
Flutter data in the transonic speed range for four nearly identical, thin, unswept wings have been o...
Two low-acceleration transonic-flutter vehicles were launched and flown. The first carried two test ...
"This report presents a survey of previous theoretical and experimental investigations on wing flutt...
Presents the results of sixty-six experimental flutter tests made on two uniform, cantilever wing mo...
The results of the basic flutter theory originally devised in 1934 and published as NACA Technical R...
Results of flutter tests on some simple all-movable-control-type models are given. One set on models...
Presented is a limited review of some experiences in flight testing of missiles and of wing flutter ...
"This report covers tests of a 5-foot model of the NACA 66,2-420 low-drag airfoil at high speeds inc...
Recent airfoil data for both flight and wind-tunnel tests have been collected and correlated insofar...
The flutter of a pitch-and-plunge airfoil (PAPA) in transonic flow is simulated using two shock-capt...
Low-speed flutter studies of a dynamically and elastically scaled model of a large multijet transpor...
NACA Research Memorandum L54D12A."September 25, 1952."Includes bibliographical references (p. 6).Mod...
Wind-tunnel flutter investigations at Mach numbers up to 0.30 have been conducted on a 40 degree swe...
A solution procedure was developed to investigate the two-dimensional, one- or two-dimensional flutt...