Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50

Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50 PDF Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 72

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Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50

Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50 PDF Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 72

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Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50 [with List of References]

Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50 [with List of References] PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 66

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Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50

Evaluation of Blended Wing-body Combinations with Curved Plan Forms at Mach Numbers Up to 3.50 PDF Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 70

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Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta and Arrow Plan Forms

Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta and Arrow Plan Forms PDF Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 82

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Investigation at Mach Numbers of 0.60 to 3.50 of Blended Wing-body Combinations with Cambered and Twisted Wings with Diamond, Delta and Arrow Plan Forms

Investigation at Mach Numbers of 0.60 to 3.50 of Blended Wing-body Combinations with Cambered and Twisted Wings with Diamond, Delta and Arrow Plan Forms PDF Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 82

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Investigation at Mach Numbers of 0.06 to 3.50 of Blended Wing Body Combinations with Cambered and Twisted Wing with Diamond, Delta and Arrow Plan Forms

Investigation at Mach Numbers of 0.06 to 3.50 of Blended Wing Body Combinations with Cambered and Twisted Wing with Diamond, Delta and Arrow Plan Forms PDF Author: George H. Holdaway
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Investigation at Mach Numbers of 0.60 to 3.50 of Blended Wing-body Combinations with Cambered and Twisted Wings with Diamond, Delta and Arrow Plan Forms [with List of References]

Investigation at Mach Numbers of 0.60 to 3.50 of Blended Wing-body Combinations with Cambered and Twisted Wings with Diamond, Delta and Arrow Plan Forms [with List of References] PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 76

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Book Description


Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta, and Arrow Plan Forms [with List of References]

Investigation at Mach Numbers of 0.20 to 3.50 of Blended Wing-body Combinations of Sonic Design with Diamond, Delta, and Arrow Plan Forms [with List of References] PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 77

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Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94

Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94 PDF Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98

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Investigation at Mach Numbers of 0.20 to 3.50 of a Blended Diamond Wing and Body Combination of Sonic Design But with Low Wave-drag Increase with Increasing Mach Number

Investigation at Mach Numbers of 0.20 to 3.50 of a Blended Diamond Wing and Body Combination of Sonic Design But with Low Wave-drag Increase with Increasing Mach Number PDF Author: George H. Holdaway
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

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