Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap PDF Download

Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap PDF full book. Access full book title Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap by Robert W. Dunning. Download full books in PDF and EPUB format.

Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap

Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap PDF Author: Robert W. Dunning
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

Get Book Here

Book Description

Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap

Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap PDF Author: Robert W. Dunning
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

Get Book Here

Book Description

Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35©, Aspect Ratio 6, Taper Ratio 0.6, and NACA 65A006 Airfoil Section

Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35©, Aspect Ratio 6, Taper Ratio 0.6, and NACA 65A006 Airfoil Section PDF Author: William C. Sleeman
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 36

Get Book Here

Book Description

Aerodynamic Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number of 4.04

Aerodynamic Characteristics of Two Delta Wings and Two Trapezoidal Wings at Mach Number of 4.04 PDF Author: Robert W. Dunning
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 24

Get Book Here

Book Description

Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body

Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body PDF Author: John R. Sevier
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44

Get Book Here

Book Description

Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94

Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94 PDF Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98

Get Book Here

Book Description

Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06

Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 PDF Author: Sleeman, Jr. (William C.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 56

Get Book Here

Book Description

The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50°

The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50° PDF Author: John B. McDevitt
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 114

Get Book Here

Book Description

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 PDF Author: Robert S. Osborne
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20

Get Book Here

Book Description

Effects at Mach Numbers of 1.61 and 2.01 of Camber and Twist on the Aerodynamic Characteristics of Three Swept Wings Having the Same Planform

Effects at Mach Numbers of 1.61 and 2.01 of Camber and Twist on the Aerodynamic Characteristics of Three Swept Wings Having the Same Planform PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52

Get Book Here

Book Description

Characteristics at Mach Number of 2.03 of a Series of Wings Having Various Spanwise Distributions of Thickness Ration and Chord

Characteristics at Mach Number of 2.03 of a Series of Wings Having Various Spanwise Distributions of Thickness Ration and Chord PDF Author: A. Warner Robins
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

Get Book Here

Book Description