Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 49
Book Description
A pressure-distribution investigation was conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the aerodynamic characteristics of a body with a fineness ratio of 8 in the two-dimensional flow field of an 8 1/3-percent-thick circular-arc wing of rectangular plan form. Data were obtained for several wing-body positions at a Mach number of 2.01 and a Reynolds number of 3,400,000 per foot.
The Aerodynamic Characteristics of a Body in the Two-dimensional Flow Field of a Circular-arc Wing at a Mach Number of 2.01
Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 49
Book Description
A pressure-distribution investigation was conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the aerodynamic characteristics of a body with a fineness ratio of 8 in the two-dimensional flow field of an 8 1/3-percent-thick circular-arc wing of rectangular plan form. Data were obtained for several wing-body positions at a Mach number of 2.01 and a Reynolds number of 3,400,000 per foot.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 49
Book Description
A pressure-distribution investigation was conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the aerodynamic characteristics of a body with a fineness ratio of 8 in the two-dimensional flow field of an 8 1/3-percent-thick circular-arc wing of rectangular plan form. Data were obtained for several wing-body positions at a Mach number of 2.01 and a Reynolds number of 3,400,000 per foot.
The Aerodynamic Characteristics of a Body in the Flow Field Near the Tip of a Circular-arc Wing of Rectangular Plan Form at a Mach Number of 2.01
Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44
Book Description
Reports and Memoranda - Aeronautical Research Council
Author: Aeronautical Research Council (Great Britain)
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 938
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 938
Book Description
Scientific and Technical Aerospace Reports
Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94
Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98
Book Description
Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing
Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards
Author: A. Warner Robins
Publisher:
ISBN:
Category : Hypersonic planes
Languages : en
Pages : 68
Book Description
Publisher:
ISBN:
Category : Hypersonic planes
Languages : en
Pages : 68
Book Description
An Experimental Investigation at a Mach Number of 2.01 of the Effects of Body Cross-section Shape on the Aerodynamic Characteristics of Bodies and Wing-body Combinations
Author: Harry W. Carlson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations. A series of 13 bodies having a given length and given longitudinal distribution of cross-sectional area but various cross-section shapes were tested at a Mach number of 2.01. The bodies were tested alone and in combination with a 47° sweptback wing having a 6-percent-thick hexagonal section.
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36
Book Description
Abstract: An experimental investigation has been performed to determine the effect of changes in body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations. A series of 13 bodies having a given length and given longitudinal distribution of cross-sectional area but various cross-section shapes were tested at a Mach number of 2.01. The bodies were tested alone and in combination with a 47° sweptback wing having a 6-percent-thick hexagonal section.
Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2
Author: William B. Igoe
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 56
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 56
Book Description
Aerodynamic Characteristics in Pitch of Several Ring-wing-body Configurations at a Mach Number of 2.2
Author: Odell A. Morris
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26
Book Description