![Pressure Distributions at Mach Numbers from 1.6 to 2.8 of 74[degree] Swept Arrow Wings with and Without Camber and Twist PDF](https://books.google.com/books/content/images/frontcover/cHhiHAAACAAJ?fife=w150-h200)
Author: Dennis F. HassonPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 74
Book Description
Pressure Distributions at Mach Numbers from 1.6 to 2.8 of 74[degree] Swept Arrow Wings with and Without Camber and Twist
![Pressure Distributions at Mach Numbers from 1.6 to 2.8 of 74[degree] Swept Arrow Wings with and Without Camber and Twist PDF](https://books.google.com/books/content/images/frontcover/cHhiHAAACAAJ?fife=w80-h100)
Author: Dennis F. HassonPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 74
Book Description
Pressure Distributions at Mach Numbers from 1.6 to 2.8 of 74 Deg Swept Arrow Wings with and Without Camber and Twist
Author: Pressure Distributions at Mach Number 2.05 on a Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber /by Harry W. Carlson
Author: Harry W. CarlsonPressure Distributions at Mach Number 2.05 on a Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber
Author: Harry W. CarlsonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44
Book Description
Aerodynamic Characteristics at Mach Numbers from 1.6 to 2.8 of 740 Swept Arrow Wings with and Without Camber and Twist
Author: Dennis F. HassonPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 42
Book Description
Pressure Distributions at Mach Number 2.05 on a Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber
Author: Harry W. CarlsonPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40
Book Description
Aerodynamic Characteristics at Mach Numbers from to 1.6 to 2.8 of 74 Deg. Swept Arrow Wings with and Without Camber and Twist
Author: Pressure Distribution at Mach Number 2.05 on a Series of Highly Swept Arrow Wings Employing Various Degrees of Twist and Camber
Author: Harry W. CarlsonAerodynamic Characteristics at Mach Numbers from 2.29 to 4.65 of 80 Deg Swept Arrow Wings with and Without Camber and Twist
Author: Off-design Aerodynamic Characteristics at Mach Numbers 1.61 and 2.20 of a Series of Highly Swept Arrow Wings Designed for Mach Number 2.0 Employing Various Degrees of Twist and Camber
Author: Wilbur D. MiddletonPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 32
Book Description