Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings

Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings PDF Author: Macon C. Ellis
Publisher:
ISBN:
Category : Aerodynamic, Supersonic
Languages : en
Pages : 44

Book Description
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.

Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings

Preliminary Investigation at Supersonic Speeds of Triangular and Sweptback Wings PDF Author: Macon C Ellis (Jr)
Publisher:
ISBN:
Category :
Languages : en
Pages : 37

Book Description


Preliminary Tests at Supersonic Speeds of Triangular and Swept-back Wings

Preliminary Tests at Supersonic Speeds of Triangular and Swept-back Wings PDF Author: Macon C. Jr Ellis
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

Book Description


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

Wind-tunnel Investigation of Damping in Roll at Supersonic Speeds of Triangular Wings at Angles of Attack PDF Author: Russell W. McDearmon
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 42

Book Description
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

Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles PDF Author: Eugene S. Love
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 104

Book Description
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.

Investigation of Bonding Between Metals and Ceramics

Investigation of Bonding Between Metals and Ceramics PDF Author: H. J. Hamjian
Publisher:
ISBN:
Category : Boron compounds
Languages : en
Pages : 696

Book Description
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.

Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 870

Book Description


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

Investigation at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles PDF Author: Eugene S. Love
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 60

Book Description


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

Investigations at Supersonic Speeds of 22 Triangular Wings Representing Twoairfoil Sections for Each of 11 Apex Angles PDF Author: Eugene S. Love
Publisher:
ISBN:
Category :
Languages : en
Pages : 60

Book Description


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

Investigations at Supersonic Speeds of 22 Triangular Wings Representing Two Airfoil Sections for Each of 11 Apex Angles PDF Author: Eugene S. Love
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description