Related Books

Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Subsonic Cruise Flight
Language: en
Pages: 33

Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Subsonic Cruise Flight

Authors: Thomas C. Kelly
Categories:
Type: BOOK - Published: 1960 - Publisher:

GET EBOOK

Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight
Language: en
Pages: 38

Aerodynamic Characteristics at Mach Numbers from 0.60 to 1.16 of a Canard Configuration Designed for Supersonic Cruise Flight

Authors:
Categories:
Type: BOOK - Published: 1960 - Publisher:

GET EBOOK

An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight
Language: en
Pages: 88

An Investigation at Mach Numbers from 0.20 to 4.63 of the Aerodynamic Performance, Static Stability, and Trimming Characteristics of a Canard Configuration Designed for Efficient Supersonic Cruise Flight

Authors:
Categories:
Type: BOOK - Published: 1961 - Publisher:

GET EBOOK

Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.50 of a Canard Configuration Having Varied Body Shapes
Language: en
Pages: 44

Aerodynamic Characteristics at Mach Numbers from 2.30 to 4.50 of a Canard Configuration Having Varied Body Shapes

Authors: Donald T. Gregory
Categories:
Type: BOOK - Published: 1959 - Publisher:

GET EBOOK

Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration
Language: en
Pages: 124

Aerodynamic Characteristics at Mach Numbers from 0.20 to 4.63 of a Canard-type Supersonic Commercial Air Transport Configuration

Authors:
Categories:
Type: BOOK - Published: 1962 - Publisher:

GET EBOOK