Author: Laurence K. Loftin
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 20
Book Description
Flutter Characteristics of Swept Wings at Transonic Speeds
Author: Laurence K. Loftin
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 20
Book Description
Theoretical Investigation of the Subsonic and Supersonic Flutter Characteristics of a Swept Wing Employing a Tuned Sting-mass Flutter Suppressor
Author: E. Carson Yates
Publisher:
ISBN:
Category : Loads (Mechanics)
Languages : en
Pages : 50
Book Description
Publisher:
ISBN:
Category : Loads (Mechanics)
Languages : en
Pages : 50
Book Description
Investigation of Wing Flutter at Transonic Speeds for Six Systematically Varied Wing Plan Forms
Author: George W. Jones
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Book Description
Results of Two Experiments on Flutter of High-aspect-ratio Swept Wings in the Transonic Speed Range
Author: William T. Lauten
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 30
Book Description
An Investigation of the Flutter Characteristics of Swept Wings at Subsonic Speeds
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
Author: Edward Carson Yates
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 58
Book Description
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 58
Book Description
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
Author: George W. Jones
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 22
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.
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 22
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.
Calculation of Flutter Characteristics for Finite-span Swept Or Unswept Wings at Subsonic, Transonic, and Supersonic Speeds by a Modified Strip Analysis
Author: Edward Carson Yates
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 494
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 494
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
Author: John R. Unangst
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 72
Book Description
Publisher:
ISBN:
Category : Flutter (Aerodynamics)
Languages : en
Pages : 72
Book Description
Comparisons of Some Wing Flutter Characteristics Obtained by Modified Strip Analysis, Subsonic Kernel Function, and Experiment
Author: Edward Carson Yates
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62
Book Description