Preliminary Investigation At Supersonic Speeds Of Triangular And Sweptback Wings

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Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings

Macon C. Ellis,Lowell E. Hasel
Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings Book PDF

Author : Macon C. Ellis,Lowell E. Hasel
Publisher : Unknown
Page : 44 pages
File Size : 49,5 Mb
Release : 1949
Category : Aerodynamic, Supersonic
ISBN : UOM:39015086494336

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Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings by Macon C. Ellis,Lowell E. Hasel Pdf

Results from a supersonic wind-tunnel investigation of a series of thin triangular and sweptback wings are presented. The triangular wing series consisted of eight triangular wings of vertex angles such that a range of leading-edge postions both inside and outside the Mach cone at the test Mach numbers of 1.43 and 1.71 was obtained. The three swept wings had angles of sweep at 45, 55, and 63 degrees and were tested at a Mach number of 1.43.

Technical Note - National Advisory Committee for Aeronautics

United States. National Advisory Committee for Aeronautics
Technical Note National Advisory Committee for Aeronautics Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 870 pages
File Size : 41,6 Mb
Release : 1949
Category : Aeronautics
ISBN : RUTGERS:39030037542356

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Technical Note - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Investigation of Bonding Between Metals and Ceramics

H. J. Hamjian
Investigation of Bonding Between Metals and Ceramics Book PDF

Author : H. J. Hamjian
Publisher : Unknown
Page : 696 pages
File Size : 55,6 Mb
Release : 1949
Category : Boron compounds
ISBN : STANFORD:36105024795903

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Investigation of Bonding Between Metals and Ceramics by H. J. Hamjian Pdf

The experiments conducted with boron carbide and each of four metals showed that nickel, cobalt, and iron formed a bonding zone between the metal and the ceramic and that chromium showed satisfactory physical wetting characteristics on the ceramic.

Annual Report - National Advisory Committee for Aeronautics

United States. National Advisory Committee for Aeronautics
Annual Report National Advisory Committee for Aeronautics Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 128 pages
File Size : 49,5 Mb
Release : 1955
Category : Aeronautics
ISBN : STANFORD:36105024166121

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Annual Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

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

Aero Digest

Anonim
Aero Digest Book PDF

Author : Anonim
Publisher : Unknown
Page : 1206 pages
File Size : 41,5 Mb
Release : 1950
Category : Aeronautics
ISBN : UOM:39015023576096

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Aero Digest by Anonim Pdf

Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack

Russell W. McDearmon
Wind tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack Book PDF

Author : Russell W. McDearmon
Publisher : Unknown
Page : 42 pages
File Size : 44,6 Mb
Release : 1956
Category : Airplanes
ISBN : UOM:39015086490169

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Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack by Russell W. McDearmon Pdf

Experimental values of the damping in roll of three triangular wings have been obtained at Mach numbers of 1.62, 1.94, 2.22, 2.41, and 2.62 over a range of angle of attack from approximately 0 to 13 degrees. The aspect ratios of the wings were 1.46, 2.31, and 3.35.

Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles

Eugene S. Love
Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles Book PDF

Author : Eugene S. Love
Publisher : Unknown
Page : 104 pages
File Size : 44,9 Mb
Release : 1949
Category : Aerodynamics, Supersonic
ISBN : UOM:39015086464453

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Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles by Eugene S. Love Pdf

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 actual test values with the nonviscous linear theory. The two series of wings had identical plan forms, a constant thickness ratio of 8 percent, a constant location of maximum-thickness point of 18 percent, and a range of apex half-angles from 10 to 45 degrees. The first series had an elliptical leading edge and the second series, a wedge leading edge. Measurements were made of lift, drag, pitching moment, and pressure distribution, the latter being confined to three wings at one Mach number.

Applied Mechanics Reviews

Anonim
Applied Mechanics Reviews Book PDF

Author : Anonim
Publisher : Unknown
Page : 810 pages
File Size : 40,8 Mb
Release : 1952
Category : Mechanics, Applied
ISBN : STANFORD:36105013125765

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Applied Mechanics Reviews by Anonim Pdf

Research Abstracts and Reclassification Notice

United States. National Advisory Committee for Aeronautics
Research Abstracts and Reclassification Notice Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 508 pages
File Size : 51,6 Mb
Release : 1954
Category : Aeronautics
ISBN : IND:30000098603164

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Research Abstracts and Reclassification Notice by United States. National Advisory Committee for Aeronautics Pdf

Research Abstracts

United States. National Advisory Committee for Aeronautics
Research Abstracts Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 442 pages
File Size : 48,6 Mb
Release : 2024-06-17
Category : Aeronautics
ISBN : OSU:32435062280326

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Research Abstracts by United States. National Advisory Committee for Aeronautics Pdf

NASA Technical Note

Anonim
NASA Technical Note Book PDF

Author : Anonim
Publisher : Unknown
Page : 616 pages
File Size : 52,7 Mb
Release : 1975
Category : Electronic
ISBN : MINN:319510008465407

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NASA Technical Note by Anonim Pdf

Technical Information Pilot

Anonim
Technical Information Pilot Book PDF

Author : Anonim
Publisher : Unknown
Page : 332 pages
File Size : 45,6 Mb
Release : 1950
Category : Science
ISBN : STANFORD:36105010854177

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Technical Information Pilot by Anonim Pdf

Index of NACA Technical Publications

United States. National Advisory Committee for Aeronautics
Index of NACA Technical Publications Book PDF

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 388 pages
File Size : 45,8 Mb
Release : 1959
Category : Aeronautics
ISBN : UCBK:C029901327

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Index of NACA Technical Publications by United States. National Advisory Committee for Aeronautics Pdf