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Flutter Characteristics of Swept Wings at Transonic Speeds

Flutter Characteristics of Swept Wings at Transonic Speeds PDF Author: Laurence K. Loftin
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 20

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Book Description

Flutter Characteristics of Swept Wings at Transonic Speeds

Flutter Characteristics of Swept Wings at Transonic Speeds PDF Author: Laurence K. Loftin
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 20

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Book Description

Theoretical Investigation of the Subsonic and Supersonic Flutter Characteristics of a Swept Wing Employing a Tuned Sting-mass Flutter Suppressor

Theoretical Investigation of the Subsonic and Supersonic Flutter Characteristics of a Swept Wing Employing a Tuned Sting-mass Flutter Suppressor PDF Author: E. Carson Yates
Publisher:
ISBN:
Category : Loads (Mechanics)
Languages : en
Pages : 50

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Book Description

Investigation of Wing Flutter at Transonic Speeds for Six Systematically Varied Wing Plan Forms

Investigation of Wing Flutter at Transonic Speeds for Six Systematically Varied Wing Plan Forms PDF Author: George W. Jones
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40

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Book Description

Results of Two Experiments on Flutter of High-aspect-ratio Swept Wings in the Transonic Speed Range

Results of Two Experiments on Flutter of High-aspect-ratio Swept Wings in the Transonic Speed Range PDF Author: William T. Lauten
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 30

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Book Description

An Investigation of the Flutter Characteristics of Swept Wings at Subsonic Speeds

An Investigation of the Flutter Characteristics of Swept Wings at Subsonic Speeds PDF Author: H. W. Hannah
Publisher:
ISBN:
Category :
Languages : en
Pages : 143

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Investigation of Transonic Flutter Characteristics of a Thin 10 Degree Sweptback Wing Having an Aspect Ratio of 4 and a Taper Ratio of 0.6

Investigation of Transonic Flutter Characteristics of a Thin 10 Degree Sweptback Wing Having an Aspect Ratio of 4 and a Taper Ratio of 0.6 PDF Author: George W. Jones
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 22

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Book Description
A flutter investigation has been made in the Langley transonic blowdown tunnel at Mach numbers between 0.79 and 1.34 on a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6. The data obtained have been compared with data from NACA Research Memorandum L55I13A for zero and 30 degree sweptback wings of the type investigated, the flutter boundary for the 10 degree sweptback wing falls between those for the zero degree and 30 degree sweptback wings in the low supersonic Mach number range. However, the subsonic level (around a Mach number of 0.8) of the flutter boundary for the 10 degree sweptback wing lies above those for the zero and 30 degree sweptback wings. In addition, the amount of rise in the flutter boundary from the subsonic level to the supersonic values is about the same for the wings with angles of sweepback of 10 degrees and zero degrees, but is much greater for the wing with an angle of sweepback of 30 degrees.

Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed

Use of Experimental Steady-flow Aerodynamic Parameters in the Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speed PDF Author: Edward Carson Yates
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 58

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Book Description

Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speeds by a Modified Strip Analysis

Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speeds by a Modified Strip Analysis PDF Author: Edward Carson Yates
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 494

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Book Description

Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6

Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6 PDF Author: John R. Unangst
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 72

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Book Description

Comparisons of Some Wing Flutter Characteristics Obtained by Modified Strip Analysis, Subsonic Kernel Function, and Experiment

Comparisons of Some Wing Flutter Characteristics Obtained by Modified Strip Analysis, Subsonic Kernel Function, and Experiment PDF Author: Edward Carson Yates
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

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Book Description