A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 1 PDF Download

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A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 1

A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 1 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100

Book Description


A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 1

A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 1 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 100

Book Description


A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings

A Viscous/potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings PDF Author: F. A. Dvorak
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 100

Book Description
An analysis method and computer program have been developed for the calculation of the viscosity dependent aerodynamic characteristics of multi-element infinite swept wings in incompressible flow. The wing configuration consisting at the most of a slat, a main element and double slotted flap is represented in the method by a large number of panels. The inviscid pressure distribution about a given configuration in the normal chord direction is determined using a two dimensional potential flow program employing a vortex lattice technique. The boundary layer development over each individual element of the high lift configuration is determined using either integral or finite difference boundary layer techniques. A source distribution is then determined as a function of the calculated boundary layer displacement thickness and pressure distributions. This source distribution is included in the second calculation of the potential flow about the configuration. Once the solution has converged (usually after 2-5 iterations between the potential flow and boundary layer calculations) lift, drag, and pitching moments can be determined as functions of Reynolds number.

A Viscous Potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 2

A Viscous Potential Flow Interaction Analysis Method for Multi-element Infinite Swept Wings, Volume 2 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 258

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 456

Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Viscous/potential Flow about Multi-element Two-dimensional and Infinite-span Swept Wings: Theory and Experiment

Viscous/potential Flow about Multi-element Two-dimensional and Infinite-span Swept Wings: Theory and Experiment PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 16

Book Description


Computer Program Abstracts

Computer Program Abstracts PDF Author:
Publisher:
ISBN:
Category : Computer programs
Languages : en
Pages : 32

Book Description


Government Reports Annual Index

Government Reports Annual Index PDF Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 882

Book Description


Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 256

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An Introductory Guide to EC Competition Law and Practice

An Introductory Guide to EC Competition Law and Practice PDF Author: Valentine Korah
Publisher:
ISBN:
Category : Antitrust law
Languages : en
Pages : 2354

Book Description


NASA Conference Publication

NASA Conference Publication PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 802

Book Description