Flow-field Characteristics and Aerodynamic Loads on External Stores Near the Fuselage and Wing-pylon Positions of a Swept-wing/fuselage Model at Mach Numbers of 0.4 and 0.7 PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Flow-field Characteristics and Aerodynamic Loads on External Stores Near the Fuselage and Wing-pylon Positions of a Swept-wing/fuselage Model at Mach Numbers of 0.4 and 0.7 PDF full book. Access full book title Flow-field Characteristics and Aerodynamic Loads on External Stores Near the Fuselage and Wing-pylon Positions of a Swept-wing/fuselage Model at Mach Numbers of 0.4 and 0.7 by R. H. Roberts. Download full books in PDF and EPUB format.
Author: R. H. Roberts
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 150
Get Book Here
Book Description
Experimental data were obtained to aid in the prediction of aerodynamic loads and separation-trajectory characteristics on stores under the influence of an aircraft flow field. Four types of data were obtained in the vicinity of a generalized aircraft model: (1) flow field surveys, using a 40-deg cone probe, to determine the local velocity field, (2) force and moment data on four store models, (3) pressure distribution data on an ogive-cylinder model, and (4) captive-trajectory store separation data on one store model. The generalized aircraft model consisted of a swept-wing/fuselage combination with rectangular, flow-through engine ducts.
Author: R. H. Roberts
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 150
Get Book Here
Book Description
Experimental data were obtained to aid in the prediction of aerodynamic loads and separation-trajectory characteristics on stores under the influence of an aircraft flow field. Four types of data were obtained in the vicinity of a generalized aircraft model: (1) flow field surveys, using a 40-deg cone probe, to determine the local velocity field, (2) force and moment data on four store models, (3) pressure distribution data on an ogive-cylinder model, and (4) captive-trajectory store separation data on one store model. The generalized aircraft model consisted of a swept-wing/fuselage combination with rectangular, flow-through engine ducts.
Author: Frederick K. Goodwin
Publisher:
ISBN:
Category : Angle of attack (Aerodynamics)
Languages : en
Pages : 210
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892
Get Book Here
Book Description
Author: Frederick K. Goodwin
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 186
Get Book Here
Book Description
The primary objective of this report is to present a prediction method for determining the forces, moments, and six-degree-of-freedom trajectories associated with stores released from single, TER, or MER configurations on fighter-bomber aircraft up to the critical speed. A secondary objective is to present important experimental results and comparison with theory from an extensive wind-tunnel test program designed to provide data to test the theory through systematic measurements of flow fields, store load distributions, store forces and moments, and captive-store trajectories.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 864
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 330
Get Book Here
Book Description
Author: Linwood W. McKinney
Publisher:
ISBN:
Category : Bomb racks
Languages : en
Pages : 28
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 952
Get Book Here
Book Description
Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 36
Get Book Here
Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 512
Get Book Here
Book Description
