Author: William T. LautenPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 30
Book Description
Results of Two Experiments on Flutter of High-aspect-ratio Swept Wings in the Transonic Speed Range
Author: William T. LautenPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 30
Book Description
Flutter Investigation of Two Thin, Low-aspect-ratio, Swept, Solid, Metal Wings in the Transonic Range by Use of Free-falling Body
Author: W. T. LautenPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18
Book Description
Flutter Characteristics of Swept Wings at Transonic Speeds
Author: Laurence K. LoftinPublisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 20
Book Description
Investigation of Wing Flutter at Transonic Speeds for Six Systematically Varied Wing Plan Forms
Author: George W. JonesPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
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. JonesPublisher:
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.
Index of NACA Technical Publications
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Book Description
WADC Technical Report
Author: United States. Wright Air Development DivisionPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1268
Book Description
Scientific and Technical Aerospace Reports
Author: Research Abstracts
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568
Book Description
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for AeronauticsPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 508
Book Description