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 PDF Download
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Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66
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Book Description
Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66
Get Book Here
Book Description
Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66
Get Book Here
Book Description
Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 152
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Book Description
Author: Frederick K. Hube
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 278
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Book Description
Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 164
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Book Description
Author: C. J. Spurlin
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 110
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Book Description
Author: Neil Arthur Zarin
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 106
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Author: Frederick K. Hube
Publisher:
ISBN:
Category :
Languages : en
Pages : 60
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Book Description
An axisymmetric, variable geometry, two-thirds scale model of a NASA Hypersonic Research Engine (HRE) inlet was tested at Mach numbers 4, 5, 6, and 8. Surface pressures and temperatures were measured on the inlet centerbody and inside the cowl. Pitot pressure measurements were made at four stations along the internal passage. The measurements were obtained for various cowl positions at free-stream Reynolds numbers from 1.08 to 5.76 million (based on a 12-in. cowl diameter) and over an angle-of-attack range from -5 to +5 deg. The model walls were internally cooled and maintained at a minimum frost-free condition at each test condition. Selected results are presented to illustrate the effects of cowl position, angle of attack, Mach number, and Reynolds number on the surface and rake station measurements. Inlet performance data at design operating conditions are also presented. (Author).
Author: James A. Behal
Publisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 692
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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.
Author: William B. Boatright
Publisher:
ISBN:
Category : Wind tunnels
Languages : en
Pages : 44
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Book Description
