Wind Tunnel Tests on a 5% Scale A3J-1 Vertical Ramp Air Inlet at Mach Numbers 1.61, 1.80 and 2.05

Wind Tunnel Tests on a 5% Scale A3J-1 Vertical Ramp Air Inlet at Mach Numbers 1.61, 1.80 and 2.05 PDF Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 152

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Wind Tunnel Tests on a 5% Scale A3J-1 Vertical Ramp Air Inlet at Mach Numbers 1.61, 1.80 and 2.05

Wind Tunnel Tests on a 5% Scale A3J-1 Vertical Ramp Air Inlet at Mach Numbers 1.61, 1.80 and 2.05 PDF Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 152

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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

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 PDF Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66

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Wind Tunnel Tests of a 5% A3J-1 Horizontal Ramp Inlet Model at Mach Numbers from Transonic to 2.25

Wind Tunnel Tests of a 5% A3J-1 Horizontal Ramp Inlet Model at Mach Numbers from Transonic to 2.25 PDF Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 164

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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

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 Author: Marion R. Bottorff
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 66

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Wind Tunnel Tests of Two-dimensional and Half-axisymmetric Inlet Models at Mach Numbers 1.5 Through 3.0

Wind Tunnel Tests of Two-dimensional and Half-axisymmetric Inlet Models at Mach Numbers 1.5 Through 3.0 PDF Author: Frederick K. Hube
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 278

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Wind Tunnel/flight Data Correlation (u).

Wind Tunnel/flight Data Correlation (u). PDF Author: James A. Behal
Publisher:
ISBN:
Category : Buffeting (Aerodynamics)
Languages : en
Pages : 692

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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

Tests of Submerged Duct Installation on a Modified Fighter Airplane in the Ames 40- by 80-foot Wind Tunnel PDF Author: Norman J. Martin
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32

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Apollo Wind Tunnel Testing Program

Apollo Wind Tunnel Testing Program PDF Author: William C. Moseley (Jr.)
Publisher:
ISBN:
Category : Aerospace engineering
Languages : en
Pages : 84

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Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive-cylinder Model at Mach Numbers 1.75 to 4.50

Wind Tunnel Tests of Rectangular Finned Variable Gap Tangent Ogive-cylinder Model at Mach Numbers 1.75 to 4.50 PDF Author: Neil Arthur Zarin
Publisher:
ISBN:
Category : Rockets (Aeronautics)
Languages : en
Pages : 106

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Longitudinal Airplane Dynamics Wind Tunnel Test Equipment

Longitudinal Airplane Dynamics Wind Tunnel Test Equipment PDF Author: O. B. Tufts
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 246

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