Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70° Swept Double-delta Wing at Mach Numbers from 2.50 to 2.86

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70° Swept Double-delta Wing at Mach Numbers from 2.50 to 2.86 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category :
Languages : en
Pages : 81

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 1.50 to 2.86

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 1.50 to 2.86 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 88

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Degree Swept Double-delta Wing at Mach Numbers Form 0.80 to 1.20, with Summary of Data from 0.20 to 6.0

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Degree Swept Double-delta Wing at Mach Numbers Form 0.80 to 1.20, with Summary of Data from 0.20 to 6.0 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category :
Languages : en
Pages : 144

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Number 0.2

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Number 0.2 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 120

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 Deg Swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 152

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Number 0.2

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Number 0.2 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 86

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 O Swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Sumary of Data from 0.20 to 6.0

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 O Swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Sumary of Data from 0.20 to 6.0 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category :
Languages : en
Pages :

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers from 0.80 to 1.20, with Summary of Data from 0.20 to 6.0 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 150

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70̊ Swept Double-delta Wing at Mach Numbers from 1.50 to 2.86

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70̊ Swept Double-delta Wing at Mach Numbers from 1.50 to 2.86 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 81

Book Description

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers 0.80 to 1.20, with Summary of Data from 0.20 to 6.0

Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊swept Double-delta Wing at Mach Numbers 0.80 to 1.20, with Summary of Data from 0.20 to 6.0 PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 145

Book Description

➤