Author: United States. Air Force. Air Matériel Command
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Book Description
Two procedures for calculating the lift distribution along the span are given, in which better account is taken of the distribution of circulation over the area than in the Prandtl lifting-line theory. The methods are also applicable to wings with sweepback. Calculated results according to two methods agree excellently. Using the second, simpler method one needs about 3 hours for the calculation of the lift distribution of a straight wing, and about eight hours for this calculation for the swept-back wing. The results are compared with those of the Multhopp method and with experimental results. Finally there is a brief not on the swept-back wing in sideslip.
The Lift Distribution of Swept-back Wings
Author: United States. Air Force. Air Matériel Command
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Book Description
Two procedures for calculating the lift distribution along the span are given, in which better account is taken of the distribution of circulation over the area than in the Prandtl lifting-line theory. The methods are also applicable to wings with sweepback. Calculated results according to two methods agree excellently. Using the second, simpler method one needs about 3 hours for the calculation of the lift distribution of a straight wing, and about eight hours for this calculation for the swept-back wing. The results are compared with those of the Multhopp method and with experimental results. Finally there is a brief not on the swept-back wing in sideslip.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Book Description
Two procedures for calculating the lift distribution along the span are given, in which better account is taken of the distribution of circulation over the area than in the Prandtl lifting-line theory. The methods are also applicable to wings with sweepback. Calculated results according to two methods agree excellently. Using the second, simpler method one needs about 3 hours for the calculation of the lift distribution of a straight wing, and about eight hours for this calculation for the swept-back wing. The results are compared with those of the Multhopp method and with experimental results. Finally there is a brief not on the swept-back wing in sideslip.
The Lift Distribution of Swept-back Wings
Author: J. Weissinger
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 48
Book Description
Note on the Calculation of the Lift Distribution of Swept Wings
Swept-back Wings with Arbitrary Lift Distribution
Author: Feodor Theilheimer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 12
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 12
Book Description
Pressure Distribution Measurements of Swept-back Wings (Second Report on Swept-back Wings)
Author: H. Luetgebrune
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 35
Book Description
Pressure distribution measurements were carried out on a straight wing, a strongly swept-back wing, and on a strongly swept forward wing. The experimental results were compared with Multhopp's theoretical lift distribution.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 35
Book Description
Pressure distribution measurements were carried out on a straight wing, a strongly swept-back wing, and on a strongly swept forward wing. The experimental results were compared with Multhopp's theoretical lift distribution.
Calculation of Lift Distribution of Swept Wings
Linearized Lifting-surface Theory for Swept-back Wings with Slender Plan Forms
Author: Harvard Lomax
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 48
Book Description
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back wing of slender plan form are developed by means of linearized lifting-surface theory. The results are applicable for all free-stream Mach numbers. The term slender implies that the ratio of the reduced span to over-all length of the wing is small.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 48
Book Description
The spanwise and chordwise distribution of loading, the lift, and the induced drag of a swept-back wing of slender plan form are developed by means of linearized lifting-surface theory. The results are applicable for all free-stream Mach numbers. The term slender implies that the ratio of the reduced span to over-all length of the wing is small.
The Spanwise Lift Distribution of Swept Wings at Subsonic Speeds
Author: Eli Herman Benstein
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 124
Book Description
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 124
Book Description