Author: Seth B. Anderson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18
Book Description
Flight tests were conducted with a light airplane equipped with a cross-wind landing gear to compare the ground distance required for take-off in calm air and with a 90 degree cross wind. These tests show that approximately 24 percent less ground run was required to attain take-off speeds of 40 to 50 miles per hour in a 16-mile-per-hour 90 degrees cross wind than in calm air.
Effect of a 90° Cross Wind on the Take-off Distance of a Light Airplane Equipped with a Cross-wind Landing Gear
Author: Seth B. Anderson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18
Book Description
Flight tests were conducted with a light airplane equipped with a cross-wind landing gear to compare the ground distance required for take-off in calm air and with a 90 degree cross wind. These tests show that approximately 24 percent less ground run was required to attain take-off speeds of 40 to 50 miles per hour in a 16-mile-per-hour 90 degrees cross wind than in calm air.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 18
Book Description
Flight tests were conducted with a light airplane equipped with a cross-wind landing gear to compare the ground distance required for take-off in calm air and with a 90 degree cross wind. These tests show that approximately 24 percent less ground run was required to attain take-off speeds of 40 to 50 miles per hour in a 16-mile-per-hour 90 degrees cross wind than in calm air.
Technical Note - National Advisory Committee for Aeronautics
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 562
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 562
Book Description
Technical Note
NASA Technical Note
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 550
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 550
Book Description
Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds
Author: John R. Spreiter
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 646
Book Description
The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 646
Book Description
The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.
Bibliography of Scientific and Industrial Reports
Technical Information Pilot
NASA Contractor Report
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1008
Book Description
Memoirs of an Aeronautical Engineer
Author: Seth B. Anderson
Publisher: National Aeronautics and Space Administration Headquarters
ISBN:
Category : Biography & Autobiography
Languages : en
Pages : 182
Book Description
Publisher: National Aeronautics and Space Administration Headquarters
ISBN:
Category : Biography & Autobiography
Languages : en
Pages : 182
Book Description
An Experimental Simulation Study of Four Crosswind Landing-gear Concepts
Author: Sandy M. Stubbs
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 66
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 66
Book Description