Investigation At Supersonic Speeds Of 22 Triangular Wings Representing Two Airfoil Sections For Each Of 11 Apex Angles
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Language: en
Pages: 104
Pages: 104
Type: BOOK - Published: 1949 - Publisher:
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: 60
Pages: 60
Type: BOOK - Published: 1955 - Publisher:
Language: en
Pages:
Pages:
Type: BOOK - Published: 1951 - Publisher:
Language: en
Pages: 60
Pages: 60
Type: BOOK - Published: 1955 - Publisher:
Language: en
Pages:
Pages:
Type: BOOK - Published: 1955 - Publisher:
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
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