A Rocket-model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail of Aspect Ratio 4.33

A Rocket-model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail of Aspect Ratio 4.33
Author :
Publisher :
Total Pages : 33
Release :
ISBN-10 : OCLC:1109643739
ISBN-13 :
Rating : 4/5 ( Downloads)
GET BOOK
Book Synopsis A Rocket-model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail of Aspect Ratio 4.33 by : Robert F. Peck

Download or read book A Rocket-model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail of Aspect Ratio 4.33 written by Robert F. Peck and published by . This book was released on 1953 with total page 33 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Rocket-model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail of Aspect Ratio 4.33 Related Books

A Rocket-model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail of Aspect Ratio 4.33
Language: en
Pages: 33

A Rocket-model Investigation of the Longitudinal Stability, Lift, and Drag Characteristics of the Douglas X-3 Configuration with Horizontal Tail of Aspect Ratio 4.33

Authors: Robert F. Peck
Categories:
Type: BOOK - Published: 1953 - Publisher:

GET EBOOK

Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60© Delta Wing and a High Unwept Horizontal Tail
Language: en
Pages: 32

Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Have a 60© Delta Wing and a High Unwept Horizontal Tail

Authors: Robert F. Peck
Categories: Delta wing airplanes
Type: BOOK - Published: 1953 - Publisher:

GET EBOOK

Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Having a 60 Degree Delta Wing and a High Unswept Horizontal Tail
Language: en
Pages: 28

Rocket-model Investigation of Longitudinal Stability and Drag Characteristics of an Airplane Configuration Having a 60 Degree Delta Wing and a High Unswept Horizontal Tail

Authors: Robert F. Peck
Categories:
Type: BOOK - Published: 1953 - Publisher:

GET EBOOK

Rocket-model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37
Language: en
Pages: 34

Rocket-model Investigation of Lateral Stability Characteristics and Power Effects of a Jet-engine Airplane Configuration with Tail Boom at Mach Numbers from 1.15 to 1.37

Authors: T. Bradley Curry
Categories: Aerodynamics
Type: BOOK - Published: 1961 - Publisher:

GET EBOOK

Lift and Drag Characteristics of the Douglas X-3 Research Airplane Obtained During Demonstration Flights to a Mach Number of 1.20
Language: en
Pages: 23

Lift and Drag Characteristics of the Douglas X-3 Research Airplane Obtained During Demonstration Flights to a Mach Number of 1.20

Authors: Donald R. Bellman
Categories: Airplanes
Type: BOOK - Published: 1954 - Publisher:

GET EBOOK

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