Author: Stanley C Perkins (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 337
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. Volume V presents the tabulated flow-field data for 6-percent thick wing model.
Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume V. Flow-Field Survey Data for the 6-Percent Thick Wing-Body Combination
Author: Stanley C Perkins (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 337
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. Volume V presents the tabulated flow-field data for 6-percent thick wing model.
Publisher:
ISBN:
Category :
Languages : en
Pages : 337
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. Volume V presents the tabulated flow-field data for 6-percent thick wing model.
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1048
Book Description
Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume II. Mach Number 0.925 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination
Author: Stanley C Perkins (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 249
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume II, presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 0.925.
Publisher:
ISBN:
Category :
Languages : en
Pages : 249
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume II, presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 0.925.
Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume III. Mach Number 0.975 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination
Author: Stanley C Perkins (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 249
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume III presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 0.975.
Publisher:
ISBN:
Category :
Languages : en
Pages : 249
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume III presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 0.975.
Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume IV. Mach Number 1.025 Flow-Field Survey Data for the 4-Percent Thick Wing-Body Combination
Author: Stanley C Perkins (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 248
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume IV presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 1.025.
Publisher:
ISBN:
Category :
Languages : en
Pages : 248
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume IV presents the tabulated flowfield data for the 4-percent thick wing model at Mach number 1.025.
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1280
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1280
Book Description
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1448
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1448
Book Description
Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume I. Summary Report, Tunnel-Empty and Mach-Number Survey Data, Force and Moment Data, and Pressure Data
Author: Stanley C Perkins (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 138
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. This report presents the data obtained during the test program conducted in the 4T and 16T Wind Tunnels at Arnold Engineering Development Center. The Flow-field data were obtained at Mach numbers 0.925, 0.975, and 1.025 and constitute the major part of the data. Volume I is a summary report which gives detailed information on the test program and presents uncertainties associated with the various types of data taken in the 4T Wind Tunnel. The volume also presents tunnel-empty and Mach-number surveys, as well as tabulated force and moment and pressure data for the Mach number range 0.80 to 1.15 and angles of attack -2, -5, 0, 2, and 5.
Publisher:
ISBN:
Category :
Languages : en
Pages : 138
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Flow velocities and static pressures were also measured near the tunnel walls to provide outer flow field information. This report presents the data obtained during the test program conducted in the 4T and 16T Wind Tunnels at Arnold Engineering Development Center. The Flow-field data were obtained at Mach numbers 0.925, 0.975, and 1.025 and constitute the major part of the data. Volume I is a summary report which gives detailed information on the test program and presents uncertainties associated with the various types of data taken in the 4T Wind Tunnel. The volume also presents tunnel-empty and Mach-number surveys, as well as tabulated force and moment and pressure data for the Mach number range 0.80 to 1.15 and angles of attack -2, -5, 0, 2, and 5.
Government Reports Annual Index: Keyword A-L
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1324
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1324
Book Description
Data Report for a Test Program to Study Transonic Flow Fields about Aircraft with Application to External Stores. Volume VI. 16T Wind Tunnel Tests
Author: Stanley C Perkins (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 106
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume VI presents data obtained for the 4-percent thick wing model in the 16T Wind Tunnel.
Publisher:
ISBN:
Category :
Languages : en
Pages : 106
Book Description
A test program was conducted to obtain measurements of flow velocities and static pressures in the vicinity of wing-body-store model (representative of a fighter-type aircraft) as well as surface pressures, forces, and moments on the model. Volume VI presents data obtained for the 4-percent thick wing model in the 16T Wind Tunnel.