Author: Donald R. Bellman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 23
Book Description
Lift and drag data were obtained during the manufacturer and Air Force demonstration flights of the Douglas X-3 airplane. The data covered the Mach number range from 0.82 to 1.20 with considerable variation in lift.
Lift and Drag Characteristics of the Douglas X-3 Research Airplane Obtained During Demonstration Flights to a Mach Number of 1.20
Author: Donald R. Bellman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 23
Book Description
Lift and drag data were obtained during the manufacturer and Air Force demonstration flights of the Douglas X-3 airplane. The data covered the Mach number range from 0.82 to 1.20 with considerable variation in lift.
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 23
Book Description
Lift and drag data were obtained during the manufacturer and Air Force demonstration flights of the Douglas X-3 airplane. The data covered the Mach number range from 0.82 to 1.20 with considerable variation in lift.
Lift and Drag Characteristics of the Douglas D-558-II Research Airplane Obtained in Exploratory Flights to a Mach Number of 2.0
Stability and Control Characteristics Obtained During Demonstration of the Douglas X-3 Research Airplane
Effect of Wing-mounted External Stores on the Lift and Drag of the Douglas D-558-II Research Airplane at Transonic Speeds
Author: Jack Nugent
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 36
Book Description
Flight Stability and Automatic Control
Author: Robert C. Nelson
Publisher: WCB/McGraw-Hill
ISBN: 9780071158381
Category : Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite
Languages : en
Pages : 441
Book Description
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Publisher: WCB/McGraw-Hill
ISBN: 9780071158381
Category : Aerodynamique / Aeronautique / Aerospatial / Automatique / Avion / Commande / Conception / Controle / Navigation / Stabilite
Languages : en
Pages : 441
Book Description
The second edition of Flight Stability and Automatic Control presents an organized introduction to the useful and relevant topics necessary for a flight stability and controls course. Not only is this text presented at the appropriate mathematical level, it also features standard terminology and nomenclature, along with expanded coverage of classical control theory, autopilot designs, and modern control theory. Through the use of extensive examples, problems, and historical notes, author Robert Nelson develops a concise and vital text for aircraft flight stability and control or flight dynamics courses.
Drag Characteristics Obtained from Several Configurations of the Modified X-15-2 Airplane Up to Mach 6.7
Comparison of Full-scale Lift and Drag Characteristics of the X-15 Airplane with Wind-tunnel Results and Theory
In-flight Lift-drag Characteristics for a Forward-swept Wing Aircraft and Comparisons with Contemporary Aircraft)
A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0
Author: Robert S. Osborne
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 20
Book Description
Introduction to Aircraft Flight Mechanics
Author: Thomas R. Yechout
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.
Publisher: AIAA
ISBN: 9781600860782
Category : Aerodynamics
Languages : en
Pages : 666
Book Description
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.