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Language: en
Pages: 104
Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles
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
Language: en
Pages:
Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles
Authors:
Eugene S. Love
Categories:
Type:
BOOK -
Published:
1951 -
Publisher:
DOWNLOAD EBOOK
Language: en
Pages: 60
Investigations at Supersonic Speeds of 22 Triangular Wings Representing Twoairfoil Sections for Each of 11 Apex Angles
Authors:
Eugene S. Love
Categories:
Type:
BOOK -
Published:
1955 -
Publisher:
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Language: en
Pages: 60
Investigation at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles
Authors:
Eugene S. Love
Categories:
Aeronautics
Type:
BOOK -
Published:
1955 -
Publisher:
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Language: en
Pages:
Annual Report - National Advisory Committee for Aeronautics
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.