Author: Albert Sherman
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 110
Book Description
Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the N. A. C. A. Variable-density Tunnel
Author: Albert Sherman
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 110
Book Description
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 110
Book Description
Interference of Wing and Fuselage from Tests of 17 Combinations in the N.A.C.A. Variable-density Tunnel Combinations with Special Junctures
Author: Albert Sherman
Publisher:
ISBN:
Category : Aiprlanes
Languages : en
Pages : 534
Book Description
As part of the wing-fuselage interferences investigation in progress in the N.A.C.A. variable-density wind tunnel, a method of eliminating the interference burble associated with critical midwing combinations was investigated. The interference burble of the critical midewing combination was shown to respond to modifications at the nose of the juncture and to be entirely suppressed with little or no adverse effect on the high-speed drag by special leading-edge fillets.
Publisher:
ISBN:
Category : Aiprlanes
Languages : en
Pages : 534
Book Description
As part of the wing-fuselage interferences investigation in progress in the N.A.C.A. variable-density wind tunnel, a method of eliminating the interference burble associated with critical midwing combinations was investigated. The interference burble of the critical midewing combination was shown to respond to modifications at the nose of the juncture and to be entirely suppressed with little or no adverse effect on the high-speed drag by special leading-edge fillets.
Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the N.A.C.A. Variable-density Tunnel
Author: Albert Sherman
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 10
Book Description
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 10
Book Description
Interference of Tail Surfaces and Wing and Fuselage from Tests of 17 Combinations in the NACA Variable-density Tunnel
Author: Albert Sherman
Publisher:
ISBN:
Category :
Languages : en
Pages : 10
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 10
Book Description
Interference of Tail Surfaces and Wing and Fuselages from Tests of 17 Combinations in the N.A.C.A. Variable-density Tunnel
Author: Albert Sherman
Publisher:
ISBN:
Category :
Languages : en
Pages : 10
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 10
Book Description
Report - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 780
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 780
Book Description
Annual Report of the National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 772
Book Description
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 772
Book Description
Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 16
Book Description
Index of Reports on Aeronautical Research
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 42
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 42
Book Description
Comparison of Vee-type and Conventional Tail Surfaces in Combination with Fuselage and Wing in the Variable-density Tunnel
Author: Harry Greenberg
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 30
Book Description
The pitching and yawing moments of a vee-type and a conventional type of tail surface were measured. The tests were made in the presence of a fuselage and a wing-fuselage combination in such a way as to determine the moments contributed by the tail surfaces. The results showed that the vee-type tail tested, with a dihedral angle of 35.3 degrees, was about 71 percent as effective in pitch as the conventional tail and had a yawing-moment to pitching-moment ratio of 0.3. The conventional tail, the panels of which were all congruent to those of the vee-type tail, had a yawing-moment to pitching-moment ratio of 0.48.These ratios are in fair agreement with values calculated by methods shown in this and previous reports. The values of the measured moments were produced from 15 to 25 percent of the calculated value by fuselage interference.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 30
Book Description
The pitching and yawing moments of a vee-type and a conventional type of tail surface were measured. The tests were made in the presence of a fuselage and a wing-fuselage combination in such a way as to determine the moments contributed by the tail surfaces. The results showed that the vee-type tail tested, with a dihedral angle of 35.3 degrees, was about 71 percent as effective in pitch as the conventional tail and had a yawing-moment to pitching-moment ratio of 0.3. The conventional tail, the panels of which were all congruent to those of the vee-type tail, had a yawing-moment to pitching-moment ratio of 0.48.These ratios are in fair agreement with values calculated by methods shown in this and previous reports. The values of the measured moments were produced from 15 to 25 percent of the calculated value by fuselage interference.