Wind-tunnel Investigation of Tapered Wings with Ordinary Ailerons and Partial-span Split Flaps PDF Download
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Author: Abe Silverstein
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 76
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Book Description
Author: Abe Silverstein
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 76
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Author: Carl Joseph Wenzinger
Publisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 9
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Author: J. B. Parkinson
Publisher:
ISBN:
Category : Seaplanes
Languages : en
Pages : 542
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Book Description
Tests were made in the N.A.C.A. tank and in the N.A.C.A. 7- by 10-foot wind tunnel of two models of transverse-step floats and three models of pointed-step floats considered to be suitable for use with single-float seaplanes. The modesl were designed at the N.A.C.A. tank as part of a program having for its object the reduction of the water resistance and spray of single-float seaplanes without reducing the angle of dead rise believed to be necessary for the satisfactory absorption of the shock loads.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 616
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages :
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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 670
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 28
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Author: Carl J. Wenzinger
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 120
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Book Description
Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 3208
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