GARTEUR High Lift Action Group: A310 flight test report. Aircraft 378

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Anlege
Annex
P. J. 1 Copy GARTEur TP042
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GARTEur Action Group AD(AG08) High Lift
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Bemerkungen
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Please find enclosed a copy of the GARTEur Report AD(AG08)
TP042: "A310 Flight Test Report".
Name Abtellung Telefon Unterschrlft Datum
nom department phone algnature date
departernent
tblephone
Dargel TE221 0421 -538-31 81 11.9.89

GARTEur LIMITED DISTRIBUTION
GARTEur TP042
GAR'TELIR HIGH LIFT ACTION GROUP AD (AGO81
A31 0 FLIGHT TEST REPORT
Aircraft 378
(F1 ight numbers 289-290-291 1
Dr. E. Greff, MBB
H. Schnieder, MBB
6. Dargel , MBB
J. Lerat, ONERA
M. Lemistre, ONERA
F. Manie, ONERA
MBB, Transport Division, Hunefeldstr. 1-5,
Bremen, West Germany
ONERA,
B.P. 72, Chat1 1 lon Cgdex, France
Bremen , ~une' 1989
- 1 -

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GARTEur TP042
SUMMARY
This report of the GARTEur Group (AG08) describes the flight test
instrumentation instal led on A310-300 MSN 378 for the High Lift Research
Flights which were performed in December 1987 at Airbus
Industries, Toulouse.
Observations during instal 1 ation, before and after flights as we1 1
as the flight test logs and a preselected set of stabilized data
points are given for further evaluation. For these time intervals
the reduced data from pressure measurements, boundary layer rakes
and hotfi lm signals were compiled and compared with wind tunnel
tests.

BERICHT/REPORT
PROGRAMM : GARTEur
Betreff:
Subject:
A310 FLIGHT TEST REPORT
Bericht Nr. / Report No.
.: Lld. Nr./ltem No.: 1
'TE2 - 1663
Wt~t.lDeor
GARTEur AD(AG08) TP042
Zusammenfassung:
Summary:
This re'port of the GARTEur Group (AG08) describes the flight test
instrumentation installed on A310-300 MSN 378 for the High Lift
Research F1 i ghts which were performed in December 1987 at Airbus
Industries, Toulouse.
Observations during instal 1 ation, before and after f 1 ights as well
as the flight test logs and a preselected set of stabilized data
points are given for further evaluation. For these time intervals
the reduced data from pressure measurements, boundary layer rakes
and hotfilm signals were compiled and compared with wind tunnel
tests.
-
Yk 4dtL
Gobilligf I Approved
........................ .......... ............
Anarkannt I Acknowledged
Vartailar I b py to:
Nmuru~ba I Rm-luua:
Datum I Data:
Bam. I Rarmrkc:
GARTEur AD (AGO8 1
Distribution List
And.-Aucp. I Rmvision: Lira I Pap: Datum I Data:
Revi sed Version June 1989
DarumIDrta: ju1 1988
- 111 -
Anr. der Liten: 309
I
Awp.lRav.No.:
Numb. of Pap:

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GARTEur TP042
CONTENTS
PAGE
I. INTRODUCTION 1
2 . DESCRIPTION OF I NSTRLIMENTATION AND A/C CONFIGURATION 3
2.1 A/CConfiguration 3
2.2 Description of Instrumentation 3
3. PARAMETER LIST 7
4. TRANSDUCER CALIBRATION 8
5. INSTALLATION ON A/C 378
5.1 Geometries/BeltDefinition
5.2 Boundary 1 ayer rakes
5.3 InstallationinsideSlatNo.2
5.4 Installation of Endevcos and Hot films
5.5 General Remarks
6. FLIGHT TEST PROGRAMME 14
7. FLIGHT LOG OF FLIGHTS NO. 289, 290, 291 15
8. SELECTION AND EVALUATION OF STABILIZED DATA POINTS 18
9. DATA REDUCTION AND EVALUATION 20
9.1 Pressure Di stri butions and Total Forces 21
9.2 Endevco Results (Static pressures 24
9.3 Boundary Layer Measurements 29
9.4 Transition Detection by Hotfilms/Endevco - Transducers 36
9.5 Attachment Line Transition (ALT) Investigation 39
1 0. CONCLUSIONS 4 2
11. REFERENCES

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TABLES
1 - 10
ILLUSTRATIONS
Chap. 1
Chap. 2
Chap. 3
Chap. 4
Chap. 5
Chap. 6
Chap. 8
Chap. 9.1
Chap. 9.2
Chap. 9.3
Chap. 9.4
Chap. 9.5
Figures 1.1 - 1.3
Figures 2.1 - 2.16
Figures 3.1 - 3.5
Figures 4.1 - 4.3
Figures 5.1 - 5.13
Figures 6.1 - 6.2
Figures 8.1 - 8.6
Figures 9.1.1 - 9.1.25
Figures 9.2.1 - 9.2.21
Figures 9.3.1 - 9.3.58
Figures 9.4.1 - 9.4.88
Figures 9.5.1 - 9.5.14