Bow Impact Loads Including the Effects of Flare

Bow Impact Loads Including the Effects of Flare PDF Author: Armin Walter Troesch
Publisher:
ISBN:
Category : Hulls (Naval architecture)
Languages : en
Pages : 86

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Bow Impact Loads Including the Effects of Flare

Bow Impact Loads Including the Effects of Flare PDF Author: Armin Walter Troesch
Publisher:
ISBN:
Category : Hulls (Naval architecture)
Languages : en
Pages : 86

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Book Description


MARAD

MARAD PDF Author: United States. Maritime Administration
Publisher:
ISBN:
Category : Merchant marine
Languages : en
Pages : 512

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Marad Publications

Marad Publications PDF Author:
Publisher:
ISBN:
Category : Shipping
Languages : en
Pages : 32

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MARAD, the Annual Report of the Maritime Administration

MARAD, the Annual Report of the Maritime Administration PDF Author: United States. Maritime Administration
Publisher:
ISBN:
Category : Merchant marine
Languages : en
Pages : 594

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Annual Report of the Maritime Administration

Annual Report of the Maritime Administration PDF Author: United States. Maritime Administration
Publisher:
ISBN:
Category : Merchant marine
Languages : en
Pages : 76

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SSC.

SSC. PDF Author: United States. Ship Structure Committee
Publisher:
ISBN:
Category : Naval research
Languages : en
Pages : 120

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The Shock and Vibration Digest

The Shock and Vibration Digest PDF Author:
Publisher:
ISBN:
Category : Shock (Mechanics)
Languages : en
Pages : 660

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Technical Note

Technical Note PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 472

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Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 280

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The Application of Green's Theorem to the Solution of Boundary-value Problems in Linearized Supersonic Wing Theory

The Application of Green's Theorem to the Solution of Boundary-value Problems in Linearized Supersonic Wing Theory PDF Author: Max A. Heaslet
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 656

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Book Description
Under the assumptions of linearized theory, general methods of solutin are given for two- and three-dimensional steady-state and two-dimensional unsteady-state equations of compressible flow. The solutions depend in all cases on the use of Green's equivalent layer of sources, sinks, and doublets. Emphasis is placed on applications in supersonic wing theory, the singularities arising in the integrations being treated by Hadamard's finite part of the technique. Four examples of different character are discussed. In particular, the load distribution over a specific swept-back lifting surface is determined at a free-stream Mach number of one.