Author: Louis P. Tosti
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 132
Book Description
Force-test Investigation of the Stability and Control Characteristics of a 1/8-scale Model of a Tilt-wing Vertical-Take-Off-and-Landing (VTOL) Airplane
Author: Louis P. Tosti
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 132
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 132
Book Description
Flight Investigation of Stability and Control Characteristics of a 1/8-scale Model of a Tilt-wing Vertical-Take-Off-and-Landing (VTOL) Airplane
Author: Louis P. Tosti
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
NASA Technical Note
Flight Investigation of the Longitudinal Stability and Control Characteristics of a Four-propeller Tilt-wing VTOL Model with a Programed Flap
Author: William A. Newsom
Publisher:
ISBN:
Category : Stability of airplanes
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Stability of airplanes
Languages : en
Pages : 32
Book Description
Force-test Investigation of the Stability and Control Characteristics of a Four-propeller Tilt-wing VTOL Model with a Programed Flap
Author: William A. Newsom
Publisher:
ISBN:
Category : Stability of airplanes
Languages : en
Pages : 60
Book Description
Publisher:
ISBN:
Category : Stability of airplanes
Languages : en
Pages : 60
Book Description
Flight-tested Investigation of Ailerons as a Source of Yaw Control on the VZ-2 Tilt-wing Aircraft
Author: Robert J. Pegg
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 28
Book Description
Slipstream Flow Around Several Tilt-wing VTOL Aircraft Models Operating Near the Ground
Author: William A. Newsom
Publisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 76
Book Description
Publisher:
ISBN:
Category : Propulsion systems
Languages : en
Pages : 76
Book Description
Stability and Control of Airplanes and Helicopters
Author: Edward Seckel
Publisher: Academic Press
ISBN: 148322015X
Category : Technology & Engineering
Languages : en
Pages : 523
Book Description
Stability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship. Comprised of 25 chapters, this book begins with a discussion on the aerodynamics of the component parts related to the lift and moment characteristics of an airplane, including wings and associated accessories; bodies such as fuselages, nacelles, and tip tanks; and control surfaces. The reader is then introduced to some mathematical techniques for linear differential equations; steady flight at different speeds; and stick force and control-free stability. Subsequent chapters focus on flaps and high-lift devices; power and compressibility effects; and the manner in which the aircraft responds to the application of control. Aeroelasticity and longitudinal equations of motion are also examined. This monograph is intended for undergraduate and graduate students taking modern engineering courses.
Publisher: Academic Press
ISBN: 148322015X
Category : Technology & Engineering
Languages : en
Pages : 523
Book Description
Stability and Control of Airplanes and Helicopters deals with aircraft flying qualities that determine the stability and control of airplanes and helicopters. It includes problems based on real aircraft, selected to represent the gamut from simple to complicated, and from conventional utility designs to futuristic research types. Many of these problems involve comparison of theory and experiment to demonstrate their mutual relationship. Comprised of 25 chapters, this book begins with a discussion on the aerodynamics of the component parts related to the lift and moment characteristics of an airplane, including wings and associated accessories; bodies such as fuselages, nacelles, and tip tanks; and control surfaces. The reader is then introduced to some mathematical techniques for linear differential equations; steady flight at different speeds; and stick force and control-free stability. Subsequent chapters focus on flaps and high-lift devices; power and compressibility effects; and the manner in which the aircraft responds to the application of control. Aeroelasticity and longitudinal equations of motion are also examined. This monograph is intended for undergraduate and graduate students taking modern engineering courses.
Force-test Investigation of the Stability and Control Characteristics of a 1/8-scale Model of a Tilt-wing Vertical-Take-Off-and-Landing (VTOL) Airplane
Author: Louis P. Tosti
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 136
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 136
Book Description
Longitudinal Aerodynamic Characteristics of a Flapped Tilt-wing Four-propeller V/stol Transport Model
Author: Kenneth W. Goodson
Publisher:
ISBN:
Category : Flaps (Airplanes)
Languages : en
Pages : 116
Book Description
Publisher:
ISBN:
Category : Flaps (Airplanes)
Languages : en
Pages : 116
Book Description