Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 152
Book Description
Wind Tunnel Tests on a 5% Scale A3J-1 Vertical Ramp Air Inlet at Mach Numbers 1.61, 1.80 and 2.05
Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 152
Book Description
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 152
Book Description
Wind Tunnel Tests of 5% Scale Vertical Ramp and Semi-conical A3J-1 Inlet Models at Mach Numbers of 1.61, 1.80 and 2.05
Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66
Book Description
Wind Tunnel Tests of a 5% A3J-1 Horizontal Ramp Inlet Model at Mach Numbers from Transonic to 2.25
Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 164
Book Description
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 164
Book Description
Wind Tunnel Tests of a 5% Scale Semi-conical A3J-1 Inlet Model at Mach Numbers of 0.9, 1.2, 1.4, 1.6, 1.8 and 2.05
Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66
Book Description
Wind Tunnel Tests of Two-dimensional and Half-axisymmetric Inlet Models at Mach Numbers 1.5 Through 3.0
Author: Frederick K. Hube
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 278
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 278
Book Description
Wind Tunnel/flight Data Correlation (u).
Author: James A. Behal
Publisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 692
Book Description
A program was conducted to obtain data, both steady state and dynamic, from wind tunnel models and full scale flight tests of the RA-5C aircraft. Data were acquired on 0.228 and 0. 125 scale RA-5C inlet models and on a fully instrumented flight test RA-5C aircraft. Interim data reports presenting the data acquired during each test have been published. These data were utilized in this report to develop scaling techniques for correlating small scale model wind tunnel data with full scale flight data. Data presented include duct steady state operating characteristics and pressure distributions in the inlet and at the engine face. Dynamic data are presented in the form of engine face turbulence contour plots, radial turbulence distributions and selected spectral data functions. Data are presented for variations of angle of attack, angle of yaw, Reynolds number, ramp angle, secondary flow rates and inlet diverter width. Brief descriptions of the model and test methods are also presented.
Publisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 692
Book Description
A program was conducted to obtain data, both steady state and dynamic, from wind tunnel models and full scale flight tests of the RA-5C aircraft. Data were acquired on 0.228 and 0. 125 scale RA-5C inlet models and on a fully instrumented flight test RA-5C aircraft. Interim data reports presenting the data acquired during each test have been published. These data were utilized in this report to develop scaling techniques for correlating small scale model wind tunnel data with full scale flight data. Data presented include duct steady state operating characteristics and pressure distributions in the inlet and at the engine face. Dynamic data are presented in the form of engine face turbulence contour plots, radial turbulence distributions and selected spectral data functions. Data are presented for variations of angle of attack, angle of yaw, Reynolds number, ramp angle, secondary flow rates and inlet diverter width. Brief descriptions of the model and test methods are also presented.
Tests of Submerged Duct Installation on a Modified Fighter Airplane in the Ames 40- by 80-foot Wind Tunnel
Author: Norman J. Martin
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Apollo Wind Tunnel Testing Program
Author: William C. Moseley (Jr.)
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 84
Book Description
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 84
Book Description
Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive-cylinder Model at Mach Numbers 1.75 to 4.50
Author: Neil Arthur Zarin
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 106
Book Description
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 106
Book Description
Longitudinal Airplane Dynamics Wind Tunnel Test Equipment
Author: O. B. Tufts
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 246
Book Description
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 246
Book Description