Characteristics of Thin Triangular Wings with Triangular-tip Control Surfaces at Supersonic Speeds with Mach Lines Behind the Leading Edge

Characteristics of Thin Triangular Wings with Triangular-tip Control Surfaces at Supersonic Speeds with Mach Lines Behind the Leading Edge
Author :
Publisher :
Total Pages : 738
Release :
ISBN-10 : STANFORD:36105024795721
ISBN-13 :
Rating : 4/5 ( Downloads)

Book Synopsis Characteristics of Thin Triangular Wings with Triangular-tip Control Surfaces at Supersonic Speeds with Mach Lines Behind the Leading Edge by : Warren A. Tucker

Download or read book Characteristics of Thin Triangular Wings with Triangular-tip Control Surfaces at Supersonic Speeds with Mach Lines Behind the Leading Edge written by Warren A. Tucker and published by . This book was released on 1948 with total page 738 pages. Available in PDF, EPUB and Kindle. Book excerpt: A theoretical analysis, based on the linearized equation for supersonic flow, of characteristics of triangular-tip control surfaces on thin triangular wings. By restriction to case for which Mach lines from wing apex lie behind the leading edge, a simplified treatment was possible; results of previous work on lift of triangular wings could be used to derive expressions for lift effectiveness, pitching moment, rolling-moment effectiveness, hinge moment due to control deflection, and hinge moment due to angle of attack. Comparisons were made with two-dimensional case.


Characteristics of Thin Triangular Wings with Triangular-tip Control Surfaces at Supersonic Speeds with Mach Lines Behind the Leading Edge Related Books

Characteristics of Thin Triangular Wings with Triangular-tip Control Surfaces at Supersonic Speeds with Mach Lines Behind the Leading Edge
Language: en
Pages: 738
Authors: Warren A. Tucker
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1948 - Publisher:

DOWNLOAD EBOOK

A theoretical analysis, based on the linearized equation for supersonic flow, of characteristics of triangular-tip control surfaces on thin triangular wings. By
The Rolling Moment Due to Sideslip of Triangular, Trapezoidal, and Related Plan Forms in Supersonic Flow
Language: en
Pages: 644
Authors: Arthur L. Jones
Categories: Aerodynamics, Supersonic
Type: BOOK - Published: 1948 - Publisher:

DOWNLOAD EBOOK

The variation of the rolling moment with sideslip and the variation of the derivative with aspect ratio and Mach number were investigated.
Index of NACA Technical Publications
Language: en
Pages: 388
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1959 - Publisher:

DOWNLOAD EBOOK

A Selected Listing of NASA Scientific and Technical Reports for ...
Language: en
Pages: 664
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1949 - Publisher:

DOWNLOAD EBOOK

Aeronautical Engineering Review
Language: en
Pages: 1908
Authors:
Categories: Aeronautics
Type: BOOK - Published: 1957 - Publisher:

DOWNLOAD EBOOK