[PDF] AGARD Advisory Report No. 138 EXPERIMENTAL DATA BASE

View - Download AGARD Advisory Report No. 138 EXPERIMENTAL DATA BASE

Previous PDF

Next PDF

NORTH ATLANTIC TREATY ORGANIZATION

ADVISORY GROW FOR AEROSPACE RESEARCH AND DEVELOPMENT (ORGANISATION DU

TRAlTE DE L'ATLANTIQUE NORD)

AGARD Advisory Report No. 138

EXPERIMENTAL DATA BASE FOR COMPUTER

PROGRAM ASSESSMENT

REPORT OF

THE FLUID DYNAMICS PANEL

WORKING GROUP

04

THE MISSION OF AGARD

The mission of AGARD is to bring together the leading personalities of the NATO nations in the fields of science

and technology relating to aerospace for the following purposes: - Exchanging of scientific and technical information;

- Continuously stimulating advances in the aerospace sciences relevant to strengthening the common defence

posture; - Improving the co-operation among member nations in a.-rospace research and development;

Providing scientific and technical advice and assistance to the North Atlantic Military Committee in the field

of aerospace research and development;

- Rendering scientific and technical assistance, as requested, to other NATO bodies and to member nations in

connection with research and development problems in the aerospace field;

- Providing assistance to member nations for the purpose of increasing their scientific and technical potential;

Recommending effective ways for the member nations to use their research and development capabilities for

the common benefit of the NATO community. The

highest authority within AGARD is the National Delegates Board consisting of officially appointed senior

representatives from each member nation. The mission of AGARD is carried out through the Panels which are

composed of experts appointed by the National Delegates, the Consultant and Exchange Programme and the Aerospace

Applications Studies Programme. The results of AGARD work are reported to the member nations and the NATO

Authorities through the AGARD series of publications of which this is one.

Participation in AGARD activities is by invitation only and is normally limited to citizens of the NATO nations.

The content of this publication has been reproduced directly from material supplied by AGARD or the authors.

Published May 1979

Copyright

O AGARD 1979

All Rights Reserved

ISBN

92-835-1323-1

Printed by Technical Editing and Reproduction Ltd

Harford House,

7-9 Charlotte St, London, WIP IHD

AGARD Advisory Report No.138

Advisory Group for Aerospace Research and

Development, NATO

EXPERIMENTAL DATA BASE FOR COMPUTER

PROGRAM ASSESSMENT

- Report of the Fluid

Dynamics Panel Working Group

04

Published May 1979

642 pages

The economical advantages of applying transonic flow technology to aircraft design has created a large number of computational methods to predict and analyse transonic flows. The proof of validity and the refinement of such methods depend primarily on experimental results. Consequently errors inherent to data generated by any individual test facility may enter the computer codes thus restricting their applicability.

P.T.O.

AGARD Advisory Report No.138

Advisory Group for Aerospace Research and

Development, NATO

EXPERIMENTAL DATA BASE FOR COMPUTER

PROGRAM ASSESSMENT - Report of the Fluid

Dynamics Panel Working Group

04

Published May 1979

642 pages

The economical advantages of applying transonic flow technology to aircraft design has created a large number of computational methods to predict and analyse transonic flows. The proof of validity and the refinement of such methods depend primarily on experimental results. Consequently errors inherent to data generated by any individual test facility may enter the computer codes thus restricting their applicability.

P.T.O. AGARD Advisory Report

No.138

Advisory Group for Aerospace Research and

Development, NATO

EXPERIMENTAL DATA BASE FOR COMPUTER

PROGRAM ASSESSMENT

- Report of the Fluid

Dynamics Panel Working Group

04

Published May 1979

642 pages

The economical advantages of applying transonic flow technology to aircraft design has created a large number of computational methods to predict and analyse transonic flows. The proof of validity and the refinement of such methods depend primarily on experimental results. Consequently errors inherent to data generated by any individual test facility may enter the computer codes thus restricting their applicability.

P.T.O.

AGARD Advisory Report

No.] 38

Advisory Group for Aerospace Research and

Development, NATO

EWERIMENTAL DATA BASE FOR COMPUTER

PROGRAM ASSESSMENT

- Report of the Fluid

Dynamics Panel Working Group

04

Published May 1979

642 pages

The economical advantages of applying transonic flow technology to aircraft design has created a large number of computational methods to predict and analyse transonic flows. The proof of validity and the refinement of such methods depend primarily on experimental results. Consequently errors inherent to data generated by any individual test facility may enter the computer codes thus restricting their applicability.

P.T.O.

AGARD-AR-I 38

Aerodynamic characteristics

Computer programs

Assessments

Mathematical models

Data processing

Aerodynamic configurations

AGARD-AR-I 38

Aerodynamic characteristics

Computer programs

Assessments

Mathematical models

Data processing

Aerodynamic configurations

AGARD-AR-138

Aerodynamiccharacteristics

Computer programs

Assessments

Mathematical models

Data processing

Aerodynamic

configurations

AGARD-AR-138

Aerodynamic characteristics

Computer programs

Assessments

Mathematical models

Data processing

Aerodynamic configurations

To aid in the development and refinement of computational methods and to improve their applicability and compatibility an EXPERIMENTAL DATA BASE was established, presenting selected test results and detailed geometric descriptions of respresentative airfoil, wing, wing-body and bodyalone confwrations. In addition, the basic limitations of the available data as well as suggestions for future tests designed to reduce these limitations are discussed in detail. ISBN

92-835-1323-1

To aid in the development and refinement of computational methods and to improve their applicability and compatibility an EXPERIMENTAL DATA BASE was established, presenting selected test results and detailed geometric descriptions of respresentative airfoil, wing, wing-body and body-alone configurations. In addition, the basic limitations of the available data as well as suggestions for future tests designed to reduce these limitations are discussed in detail. ISBN 92-835-1323-1 To aid in the development and refinement of computational methods and to improve their applicability and compatibility an EXPERIMENTAL DATA BASE was established, presenting selected test results and detailed geometric descriptions of respresentative airfoil, wing, wing-body and body-alone configurations. In addition, the basic limitations of the available data as well as suggestions for future tests designed to reduce these limitations are discussed in detail. ISBN

92-835-1323-1

To aid in the development and refinement of computational methods and to improve their applicability and compatibility an EXPERIMENTAL DATA BASE was established, presenting selected test results and detailed geometric descriptions of respresentative airfoil, wing, wing-body and body-alone configurations. In addition, the basic limitations of the available data as well as suggestions for future tests designed to reduce these limitations are discussed in detail. ISBN

92-835-1323-1

Telephone 746.0810 . Telex 610176

I

NATO <$ OTAN

7 RUE ANCELLE 92200 NEUILLY-SUR.SEINE

FRANCE

AGARD does NOT huld stocks of AGARD publications at the above address for general distribution. Initial distribution of AGARD

publications

is made tu AGARD Member Nations through the following National Distribution Centres. Further copies are sometimes available

from these Centres, but if not may be purchased in Microfiche or Photocopy form from the Purchase Agencies listed below.

NATIONAL

DISTRIBIITION CENTRES

BELGIUM ITALY

Cuordunnateur A(;ARU VSL Aeronautic2 Militare

ktat-Major de la Force ACrienne Ufticio del Delegato Nazionale all'ACARD

Quartier Reine Elisabeth 3, Piarzale Adenauer

Rue d'Evere. 1140 Uruxelles RumaiEtJR

CANADA LUXEMBOURG

Defence Scientific Information Scrvice See Belgium Department of Natiunal Defence

Ottawa, Ontario KIA 022 NETHERLANDS Netherlands Delegation to AGARD DENMARK National Aerospace Laboratory, NLR

Danish Defence Research

Buard P.O. Box 126

Qsterbrogades Kaserne Delft

Cupenhagen

0

NORWAY FRANCE

Nonvcgian Defence Research Establishment

O.N.E.R.A.

(Directiun) Main Library

29 Avenue de la Division Leclerc

P.O. Box 25

92 Ch=tillun sous Bagneux

N-2007 KjeUer

a

DISTRIBUTION OF UNCLASSIFIED

AGARD PUBLICATIONS

GIKMANY PORTUGAL

Zcntralstellc fur Luft. und Raumfahrt-

Direcfao do Servifa de Material

dokumentation und -informatiun da Forca Aerea cia Fachinformationr~entrum Energie, Rua da Escola Politecnica 42

Pllysik, Mathematik GmbH Lisbaa

Kernforschungs~entrum Attn: ACARD National Delegate 75

14 Eggenstein-Leopuldshafen 2 TURKEY GREECE Department of Research and Development (ARGE) Hellenic Air Force

General Staff Ministry of National Defence, Ankara Research and Development Directorate

Holargos. Athens, Greece UNITED KINGDOM Defence Research Information Centre ICELAND Station Square House

Director

of Aviation St. Mary Cray c/o Flugrad

Orpington. Kent BR5 3RE Reykjavik UNITED STATES

National Aeronautics and Space Administration (NASA)

Langley Field, Virginia 23365

Attn: Report Distribution and Storage Unit

IIII I \111.1JS1.\1l.SN\~10Y41. UISTKIBI'TIOS( khTRI I\'.%S\IUO~S UOTllOLI)

5TOChS Ol AIo.\KIJ I'I BLI('4TIO\S. A>I) APPI.IChTIOYS I.ORCOPltS 51101~LI) Hf' %IAl)t

L~IINational Technical

Information Service (NTIS) 5285 Port

Royal Road

Springfield

Virginia 22161, USA PURCHASE AGENCIES

Microtiche

Space Documentation Service European Space Agency

10, rue Mario Nikis

75015 Paris. France Microfiche

Technology Reports

Centre

(DTI)

Station Square House

St. Mary Cray

Orpington, Kent BRS 3RF

England

Requests

for microtiche or photocopies of ACARD documents should include the AGARD serial number, title, author or editor, and

publication date. Requests to NTIS should include the NASA accession report number. Full bibliographical references and abstracts of ACARD publications are given in the following journals: I

Scientific and Technical Aerospace Reports (STAR) Government Reports Announcements (GRA) published by NASA Scientific

and Technical published by the

Nations1 Technical

k Information Facility Information Services, Springfield

Post Office Box 8757 Virginia 22161. USA

Ballimore!Washington International Airport Maryland

2 1240: USA

finfed b.v Tecknicnl Editingand Reproduerion Lrd

Horfijrd House, 7-9 Chorlorre Sr. London WIP IHD

ISBN 72-335-1323-1

REPORT DOCUMENTATION PAGE

1.Recipient's Reference 3. Further Reference

ISBN 92-835-1323-1 2.0riginator's Reference

AGARD-AR-138 4.Security Classification of Document

UNCLASSIFIED

S.Originator Advisory Group for Aerospace Research and Development

North Atlantic Treaty Organization

7 rue Ancelle, 92200 Neuilly

sur Seine, France

6.Title

EXPERIMENTAL DATA BASE FOR COMPUTER PROGRAM ASSESSMENT - Report of the Fluid Dynamics Panel Working Group 04

7.Resented at

8. Author(s)

Various

10.Author's Address

Various

9.Date

May 1979

11.Pages

624 pages

12.DistributionStatement

This document is distributed in accordance with AGARD policies and regulations, which are outlined on the

Outside Back Covers of all AGARD publications

13.Keywords/Descriptors

Aerodynamic characteristics Mathematical models

Computer programs Data processing

Assessments

Aerodynamic configurations

14. Abstract

The economical advantages of applying transonic flow technology to aircraft design has created a large number of computational methods to predict and analyse transonic flows. The proof of validity and the refinement of such methods depend primarily on experimental results. Consequently errors inherent to data generated by any individual test facility may enter the computer codes thus restricting their applicability. To aid in the development and refinement of computational methods and to improve their applicability and compatibility an EXPERIMENTAL DATA BASE was established, presenting selected test results and detailed geometric descriptions of representative airfoil, wing, wing-body and body-alone configurations. In addition, the basic limitations of the available data as well as suggestions for future tests designed to reduce these limitations are discussed in detail. The economical advantages of applying transonic flow technology to aircraft design has created a large number of computational methods to predict and analyse transonic flows. The proof of validity and the refinement of such methods depend primarily on experimental results. Consequently errors inherent to data generated by any individual test facility may enter the computer codes thus restricting their applicability. To aid in the development and refinement of computational methods and to improve their applicability and compatibility an EXPERIMENTAL DATA BASE was established, presenting selected test results and detailed geometric descriptions of representative airfoil, wing, wing-body and body-alone confgurations. In addition, the basic limitations of the available data as well as suggestions for future tests designed to reduce these limitations are discussed in detail.

Professor Dr.

J.BARCHE

Chairman

Fluid Dynamics Panel Working

Group 04

CONTENTS

PREFACE

by

J.Barche

Page iii

Reference

INTRODUCTION AND OVERVIEW OF CONFIGURATIONS

by

J.Barche

LIMITATIONS OF AVAILABLE DATA

by

T.W.Binion

RECOMMENDATIONS FOR FUTURE TESTING

by

K.G.Winter and L.H.Ohman

CONCLUDING REMARKS

by

J.Barche

APPENDIX A - 2-D CONFIGURATIONS

by J .Sloof

NACA 0012 AIRFOIL

by

J.J.Thibert, M.Grandjacques and L.H.Ohman

NLR QE 0.1 1 - 0.75 - 1.375 AIRFOIL

by NLR and NAE

SUPERCRITICAL AIRFOIL CAST

7 SURFACE PRESSURE, WAKE AND BOUNDARY

LAYER MEASUREMENTS

by EStanewsky, W.Puffert, R.MuUer and T.E.B.Bateman

NLR 7301 AIRFOIL

by NLR Amsterdam

AIRFOIL SKF

1 .l. WITH MANEUVER FLAP

by

E.Stanewsky and J .J .Thibert

AEROFOIL RAE 2822 - PRESSURE DISTRIBUTIONS, AND BOUNDARY LAYERquotesdbs_dbs27.pdfusesText_33

[PDF] les différents types de bases de données

[PDF] base de données pdf

[PDF] nature du solide

[PDF] nombre d'arête d'un cylindre

[PDF] base d'un solide définition

[PDF] nature des faces

[PDF] nom d'une base

[PDF] les solides faces aretes sommets

[PDF] définition équité scolaire

[PDF] communication écrite pdf

[PDF] les étapes d une planification stratégique

[PDF] biochimie pour les nuls

[PDF] biochimie pdf livre

[PDF] cours biochimie générale gratuit

[PDF] la mise en place d'une base de données