Cover Image

Simultaneous triangularization /

Show other versions (1)

It is essentially self-contained modulo solid courses in linear algebra (for the first half) and functional analysis (for the second half), and is therefore suitable as a text or reference for a graduate course."--BOOK JACKET.

Bibliographic Details
Main Author:	Radjavi, Heydar
Corporate Author:	SpringerLink (Online service)
Other Authors:	Rosenthal, Peter, 1941-
Format:	eBook
Language:	English
Published:	New York : Springer, [2000]
Series:	Universitext
Subjects:	Triangularization (Mathematics) Triangularisation (Mathématiques) Dreieckszerlegung. Lineare Transformation. Electronic books.
Online Access:	Connect to the full text of this electronic book

Similar Items

Simultaneous triangularization /
by: Radjavi, Heydar
Published: (2000)

Triangulations and applications /
by: Hjelle, Øyvind
Published: (2006)

On nearly triangular matrices /
by: Ostrowski, A. M. (Alexander Markowich), 1893-1986
Published: (1952)

Triangulations : structures for algorithms and applications /
by: De Loera, Jesús A., 1966-
Published: (2010)

Triangular norms /
by: Klement, E. P. (Erich Peter)
Published: (2000)

Ideals in triangular AF algebras /
by: Hudson, Timothy Dean, 1964-
Published: (1992)

The Delta wing : history and development /
by: Lippisch, Alexander, 1894-1976
Published: (1981)

The Jacobson radical of triangular AF algebras /
by: Donsig, Allan Paul, 1964-
Published: (1993)

Complementary triangular forms for pairs of matrices and operators /
by: Zuidwijk, Rob
Published: (1994)

Some exploratory measurements of leading-edge vortex positions on a delta wing oscillating in heave /
by: Maltby, R. L.
Published: (1965)

Flight measurements of the elevator and aileron hinge-moment derivatives of the Fairey Delta 2 aircraft up to a Mach number of 1.6 and comparisons with wind-tunnel results /
by: Rose, Robert
Published: (1967)

Measurements : at Mach numbers up to 2.8, of the longitudinal characteristics of one plane and three cambered slender 'ogee' wings /
by: Taylor, C. R.
Published: (1963)

Heat-transfer and pressure measurements on the upper surface of a delta wing at incidence at Mach numbers between 2.0 and 3.6 /
by: Edwards, J. B. W.
Published: (1967)

Properties of a two-paramenter family of thin conically cambered delta wings by slender-body theory /
by: Cooke, J. C. (John Caister)
Published: (1962)

Pressure distributions and flow patterns at M = 4.0 on some delta wings /
by: Squire, Leonard Charles
Published: (1964)

A theoretical investigation for delta wings with leading-edge separation at low speeds /
by: Nangia, R. K.
Published: (1970)

Effects of wing stiffness and inertia changes on the modes and frequencies of a model delta aircraft /
by: Webb, D. R. B.
Published: (1962)

A three component gun tunnel balance designed for testing thin delta wings /
by: Opatowski, T.
Published: (1971)

Calculations of the effects of blowing from the leading edges of a cambered delta wing /
by: Barsby, J. E.
Published: (1978)

Low-speed wind-tunnel experiments on a series of sharp-edged delta wings /
by: Earnshaw, P. B.
Published: (1966)

Measurements of the direct pitching oscillation derivatives for three cropped delta and three arrowhead planforms at subsonic and transonic speeds /
by: Miles, C. J. W.
Published: (1965)

Measurements of the pitching-moment derivatives on a sharp-edged delta wing in incompressible flow /
by: Woodgate, L.
Published: (1964)

The airforces on the low-aspect-ratio rectangular wing oscillating in sonic flow /
by: Davies, David Eric
Published: (1963)

Analysis of the static pressure distribution on a Delta wing in subsonic flow /
by: Kirkpatrick, David L. I.
Published: (1970)

Investigation of the normal force characteristics of slender delta wings with various rhombic cross-sections in subsonic conical flow /
by: Kirkpatrick, David L. I.
Published: (1967)

An experimental investigation of the structure of a leading-edge vortex /
by: Earnshaw, P. B.
Published: (1962)

Pressure measurements on a model delta wing undergoing oscillatory deformation /
by: Lambourne, N. C.
Published: (1972)

An investigation of the flow about a plane half-wing of cropped-delta planform and 6 per cent symmetrical section at stream Mach numbers between 0.8 and 1.41 /
by: Rogers, E. W. E.
Published: (1962)

Low-speed wind-tunnel measurements on a thin sharp-edged delta wing with 70 leading-edge sweep : with particular reference to the position of leading-edge-vortex breakdown /
by: Lawford, J. A.
Published: (1963)

Delta wings with longitudinal camber at low speed /
by: Nangia, R. K.
Published: (1970)

Experimental investigation of the positions of the leading-edge vortices above slender delta wings with various rhombic cross-sections in subsonic conical flow /
by: Kirkpatrick, David L. I.
Published: (1967)

Measurements of the effects of thickness on vortex breakdown position on a series of sharp-edged delta wings /
by: Earnshaw, P. B.
Published: (1968)

Analysis of the zero-lift wave drag measured on delta wings /
by: Weber, J.
Published: (1978)

The dynamic stability derivatives of a slender wing : a comparison of theory with free-flight model tests at near-zero lift, M = 0.8 to 2.4 /
by: Turner, K. J.
Published: (1968)

Flight determination of wing flow patterns and buffet boundaries for the Fairey Delta 2 aircraft at Mach numbers between 0.4 and 1.3 : and comparison with wind tunnel results /
by: Dee, F. W.
Published: (1967)

Wind tunnel tests and theoretical investigations on the effect of a localised mass on the flutter of a delta wind with fixed root /
by: Donno, G. F.
Published: (1962)

The use of conical camber to produce flow attachment at the leading edge of a delta wing and to minimize life-dependent drag at sonic and supersonic speeds /
by: Smith, Jeremy H. B.
Published: (1963)

Some observations of the flow over a deltawinged model with 55-deg leading-edge sweep, at Mach numbers between 04 and 18 /
by: Sutton, E. P.
Published: (1960)

Free-flight measurements of pressure and heat transfer on a blunt leading-edge caret wing at design and off-design mach numbers (M [infinity] =0.9 to 3.36) /
by: Greenwood, G.H
Published: (1971)

Measurements of skin friction on a cambered delta wing at supersonic speeds /
by: Winter, Kenneth George
Published: (1967)