Related Books

Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles
Language: en
Pages: 104
Authors: Eugene S. Love
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1949 - Publisher:

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The results of tests of 11 triangular wings were conducted at Mach numbers 1.62, 1.92, and 2.40 to determine the effect of leading-edge shape and to compare act
Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles
Language: en
Pages:
Investigations at Supersonic Speeds of 22 Triangular Wings Representing Twoairfoil Sections for Each of 11 Apex Angles
Language: en
Pages: 60
Investigation at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles
Language: en
Pages: 60
Authors: Eugene S. Love
Categories: Aeronautics
Type: BOOK - Published: 1955 - Publisher:

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Annual Report - National Advisory Committee for Aeronautics
Language: en
Pages:
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1955 - Publisher:

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Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.