EUROSHOCK: drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995
Gespeichert in:
| Format: | Buch |
|---|---|
| Sprache: | German |
| Veröffentlicht: |
Braunschweig [u.a.]
Vieweg
1997
|
| Schriftenreihe: | Notes on numerical fluid mechanics
56 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Literaturangaben |
| Beschreibung: | 414 S. graph. Darst. 23 cm |
| ISBN: | 3528076569 |
Internformat
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| 245 | 1 | 0 | |a EUROSHOCK |b drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 |c ed. by Egon Stanewsky ... |
| 264 | 1 | |a Braunschweig [u.a.] |b Vieweg |c 1997 | |
| 300 | |a 414 S. |b graph. Darst. |c 23 cm | ||
| 336 | |b txt |2 rdacontent | ||
| 337 | |b n |2 rdamedia | ||
| 338 | |b nc |2 rdacarrier | ||
| 490 | 1 | |a Notes on numerical fluid mechanics |v 56 | |
| 490 | 0 | |a Community research in aeronautics | |
| 500 | |a Literaturangaben | ||
| 650 | 4 | |a Boundary layer control |x Research |z European Union countries | |
| 650 | 4 | |a Drag (Aeronautics) |x Research |z European Union countries | |
| 650 | 4 | |a Shock waves |x Research |z European Union countries | |
| 650 | 4 | |a Transonic planes |x Wings |x Design and construction | |
| 650 | 4 | |a Transonic planes |x Wings |x Research |z European Union countries | |
| 650 | 0 | 7 | |a Stoß-Grenzschicht-Wechselwirkung |0 (DE-588)4282522-2 |2 gnd |9 rswk-swf |
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| 650 | 0 | 7 | |a Kompressible Strömung |0 (DE-588)4032018-2 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Transsonische Strömung |0 (DE-588)4135633-0 |2 gnd |9 rswk-swf |
| 650 | 0 | 7 | |a Widerstandsverminderung |0 (DE-588)4210098-7 |2 gnd |9 rswk-swf |
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Datensatz im Suchindex
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| adam_text |
TABLE
OF
CONTENTS
PAGE
A
SYNOPSIS
OF
THE
PROJECT
EUROSHOCK,
E.
STANEWSKY,
DLR,
J.
DTFERY,
ONERA,
J.
FULKER,
DERA,
AND
W.
GEIFLLER,
DLR
.
1
1
INTRODUCTION
.
3
2
BASIC
EXPERIMENTS
AND
PHYSICAL
MODELING
.
6
2.1
TWO-DIMENSIONAL
SHOCK
CONTROL
.
7
2.1.1
TEST
SET-UP
FOR
THE
BASIC
EXPERIMENTS
.
7
2.1.2
THE
PERFORATED
PLATES
.
8
2.1.3
EFFECT
OF
PLATE
GEOMETRY
ON
SHOCK
CONTROL
EFFECTIVENESS
.
11
2.1.4
BOUNDARY
LAYER
DEVELOPMENT
OVER
THE
CAVITY
REGION
.
13
2.1.5
ASSESSMENT
OF
TURBULENCE
MODELS
AND
SHOCK
CONTROL
LAWS
.
16
2.2
THREE-DIMENSIONAL
SHOCK
CONTROL
.
19
2.2.1
EXPERIMENTAL
ARRANGEMENT
AND
PROCEDURE
.
19
2.2.2
ANALYSIS
OF
EXPERIMENTAL
RESULTS
.
21
2.2.3
NUMERICAL
SIMULATION
OF
THE
INTERACTION
.
23
2.3
CONCLUSION
AND
FUTURE
WORK
.
25
3
EXTENSION
OF
NUMERICAL
METHODS
AND
PRELIMINARY
CONTROL
ASSESSMENT
.
26
3.1
BASIC
NUMERICAL
METHODS
.
26
3.2
PRE-COMPUTATIONS
WITHOUT
CONTROL
.
28
3.2.1
STEADY
FLOW
PRE-COMPUTATIONS
FOR
THE
AIRFOIL
DA
LVA-1
A
.
29
3.2.2
UNSTEADY
FLOW
PRE-COMPUTATIONS
.
31
3.3
EXTENSION
OF
THE
NUMERICAL
CODES
TO
SHOCK
CONTROL
.
32
3.4
COMPUTATIONAL
RESULTS
FOR
AIRFOIL
FLOW
WITH
CONTROL
.
34
3.4.1
AIRFOIL
DRA
2303
-
STEADY
FLOW
CONDITIONS
.
35
3.4.2
AIRFOIL
DRA
2303
-
UNSTEADY
FLOW
CONDITIONS
.
38
3.4.3
AIRFOIL
DA
LVA-1
A
WITH
AND
WITHOUT
CONTROL
.
41
3.4.4
AIRFOIL
VA-2
WITH
PASSIVE
AND
ACTIVE
CONTROL
.
45
3.5
CONCLUSION
AND
FUTURE
WORK
.
49
4
AIRFOIL
TESTS
WITH
AND
WITHOUT
CONTROL
.
50
4.1
EXPERIMENTAL
PROGRAM
.
50
4.2
EXPERIMENTS
WITH
THE
AIRFOIL
DA
LVA-1
A
.
50
4.2.1
AIRFOIL
CHARACTERISTICS
AND
WIND
TUNNEL
MODEL
.
50
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
4.2.2
WIND
TUNNEL
CHARACTERISTICS
.
54
4.2.3
DISCUSSION
OF
T2
RESULTS
.
54
4.2.4
DISCUSSION
OF
KRG
RESULTS
.
59
4.3
EXPERIMENTS
WITH
THE
AIRFOIL
DRA
2303
.
62
4.3.1
AIRFOIL
CHARACTERISTICS
AND
WIND
TUNNEL
MODEL
.
62
4.3.2
WIND
TUNNEL
CHARACTERISTICS
.
63
4.3.3
DISCUSSION
OF
STEADY
RESULTS
.
63
4.3.4
CONTROL
EFFECT
ON
BUFFET
.
65
4.4
EXPERIMENTS
WITH
THE
AIRFOIL
VA-2
.
67
4.4.1
AIRFOIL
CHARACTERISTICS
AND
WIND
TUNNEL
MODEL
.
68
4.4.2
WIND
TUNNEL
CHARACTERISTICS
.
69
4.4.3
COMPARISON
OF
PRESENT
AND
EARIIER
RESULTS
.
69
4.4.4
EFFECT
OF
PASSIVE
AND
ACTIVE
CONTROL
.
69
4.5
CONCLUSION
AND
FUTURE
WORK
.
74
5
ASSESSMENT
OF
SHOCK
CONTROL
-
A
SUMMARY
.
76
6
OVERALL
CONCLUSION
AND
FUTURE
WORK
.
78
7
REFERENCES
.
79
B
INDIVIDUAL
CONTRIBUTION
.
83
8
INTRODUCTION
TO
THE
INDIVIDUAL
CONTRIBUTIONS,
E.
STANEWSKY,
DLR
.
85
9
BASIC
STUDY
OF
PASSIVE
CONTROL
APPLIED
TO
A
TWO-DIMENSIONAL
TRANSONIC
INTERACTION,
R.
BUR,
J.
DDLERY
AND
B.
CORBEL,
ONERA
.
89
9.1
INTRODUCTION
.
89
9.2
EXPERIMENTAL
CONDITIONS
.
90
9.2.1
TEST
SET-UP
ARRANGEMENT
.
90
9.2.2
TECHNIQUES
OF
INVESTIGATION
AND
DATA
PROCESSING
.
91
9.2.3
CONFIGURATIONS
TESTED
.
;
.
93
9.3
EXPERIMENTAL
RESULTS
.
94
9.3.1
FLOW
VISUALIZATIONS
.
94
9.3.2
SURFACE
PRESSURE
DISTRIBUTIONS
.
95
9.3.3
MEAN
FLOW
FIELD
PROPERTIES
.
97
9.3.4
TURBULENT
FIELD
PROPERTIES
.
101
9.3.5
TOTAL
DRAG
COEFFICIENT
IN
THE
CONTROL
REGION
.
104
9.3.6
PERFORATED
PLATES
EXCRESCENCE
DRAG
.
105
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
9.4
THEORETICAL
STUDY
.
106
9.4.1
NUMERICAL
APPROACH
.
106
9.4.2
SURFACE
PRESSURE
DISTRIBUTIONS
.
107
9.4.3
TRANSPIRATION
VELOCITY
DISTRIBUTIONS
.
108
9.5
CONCLUSION
.
109
9.6
REFERENCES
.
110
10
PASSIVE
CONTROL
OF
SHOCK
WAVE
-
BOUNDARY
LAYER
INTERACTION
AND
POROUS
PLATE
TRANSPIRATION
FLOW,
R.
BOHNING
AND
P.
DOERFFER,
UNIVERSITY
OF
KARLSRUHE
.
113
10.1
INTRODUCTION
.
113
10.2
POROUS
PLATE
FLOW
.
114
10.2.1
MEASUREMENTS
.
114
10.2.2
EFFECTIVE
FLOW
WITHIN
A
HOLE
AND
PRESSURE
DROP
THROUGH
THE
POROUS
PLATE
.
115
10.2.3
IMPLEMENTATION
OF
THE
POROUS
PLATE
FLOW
MODEL
.
118
10.3
EXPERIMENTAL
INVESTIGATION
OF
SHOCK
BOUNDARY
LAYER
INTERACTION
WITH
PASSIVE
CONTROL
.
119
10.3.1
INTRODUCTION
.
119
10.3.2
MACH
NUMBER
AT
THE
WALL
.
120
10.3.3
BOUNDARY
LAYER
PROFILES
WITHOUT
PASSIVE
CONTROL
.
121
10.3.4
PASSIVE
CONTROL
EFFECT
.
121
10.4
NUMERICAL
SIMULATION
OF
SBLIC
.
123
10.4.1
NUMERICAL CODE
.
123
10.4.2
RESULTS
.
123
10.5
REFERENCES
.
124
11
AN
INVESTIGATION
OF
PASSIVE
CONTROL
APPLIED
TO
SWEPT
SHOCK-WAVE/
BOUNDARY
LAYER
INTERACTIONS,
L.C.
SQUIRE,
A.F.K.
YEUNG
AND
X.
FAUCHER,
UNIVERSITY
OF
CAMBRIDGE
.
135
11.1
INTRODUCTION
.
135
11.2
EXPERIMENTAL
APPARATUS
.
136
11.3
COMPUTATIONAL
METHOD
.
137
11.4
RESULTS
AND
DISCUSSION
.
138
11.4.1
INTERACTION
WITHOUT
PASSIVE
CONTROL
.
138
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
11.4.2
INTERACTION
WITH
PASSIVE
CONTROL
.
138
11.5
CONCLUSIONS
.
140
11.6
REFERENCES
.
141
12
NUMERICAL
INVESTIGATION
OF
THE
PASSIVE
SHOCK
CONTROL
ON
TRANSONIC
AIRFOILS
THROUGH
AN
EULER/BOUNDARY-LAYER
COUPLING
TECHNIQUE,
P.
DE
MATTEIS
AND
C.
DIMA,
CIRA
.
151
12.1
INTRODUCTION
.
151
12.2
EXTENSION
OF
THE
EUBL2D
METHOD
TO
PASSIVE
SHOCK
CONTROL
CALCULATIONS
.
152
12.3
CALCULATION
OF
THE
TRANSPIRATION
VELOCITY
.
155
12.4
NUMERICAL
RESULTS
.
156
12.4.1
VALIDATION
OF
THE
METHOD
.
157
12.4.2
NUMERICAL
ASSESSMENT
OF
PASSIVE
CONTROL
.
157
12.5
CONCLUSIONS
.
160
12.6
REFERENCES
.
161
13
INTRODUCTION
OF
PASSIVE
SHOCK
CONTROL
IN
AN
INTERACTIVE
BOUNDARY
LAYER
METHOD,
C.
DE
NICOLA,
UNIVERSITY
OF
NAPLES
.
171
13.1
INTRODUCTION
.
171
13.2
INVISCID
FLOW
SOLVER
.
172
13.3
VISCOUS
SOLVER
.
172
13.4
TRANSPIRATION
MODEL
.
173
13.5
DESIGN
OF
THE
CAVITY
LOCATION
.
173
13.6
CALCULATION
OF
TOTAL
DRAG
.
173
13.7
WAKE
EFFECT
.
174
13.8
RESULTS
.
174
13.8.1
BLOCK
DECOMPOSITION
AND
LGR
CONCEPT
.
174
13.8.2
NEW
CORRELATION
FOR
A
VENTILATED
BOUNDARY
LAYER
.
175
13.8.3
TEST
CASES
FOR
THE
AIRFOIL
DRA
2303
WITH
AND
WITHOUT
CONTROL
.
177
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
13.8.4
TEST
CASES
FOR
THE
AIRFOIL
DA-LVA-1A
WITH
AND
WITHOUT
CONTROL
.
188
13.8.5
TEST
CASES
FOR
THE
AIRFOIL
VA-2
WITH
AND
WITHOUT
CONTROL
.
190
13.8.6
TEST
CASE
FOR
THE
VA-2
AIRFOIL
AT
0.75
C|
0.85
WITH
AND
WITHOUT
CONTROL:
A
SUMMARY
.
192
13.9
CONCLUSION
.
194
13.10
REFERENCES
.
194
14
EXTENSION,
VALIDATION
AND
APPLICATION
OF
THE
DA
VII
TRANSONIC
AIRFOIL
CODE
WITH
PASSIVE
SHOCK
CONTROL,
G.
DARGEL,
DAIMLER-BENZ
AEROSPACE
AIRBUS
GMBH
.
195
14.1
INTRODUCTION
.
195
14.2
BASIC
AIRFOIL
FLOW
PREDICTION
METHOD
.
195
14.2.1
EQUIVALENT
INVISCID
FLOW
AND
VISCOUS
BOUNDARY
CONDITIONS
.
196
14.2.2
INTERACTIVE
BOUNDARY
LAYER
AND
COUPLING
METHOD
.
196
14.2.3
FORCES
.
197
14.3
EXTENSION
OF
THE
VII
METHOD
TO
PASSIVE
SHOCK
CONTROL
.
197
14.3.1
SC
LAW
PROCEDURE
.
198
14.3.2
MODIFICATIONS
OF
THE
VISCOUS
SOLVER
.
200
14.3.3
MODIFICATION
OF
THE
SOLUTION
PROCEDURE
.
201
14.3.4
GRID
ADAPTATION
.
202
14.4
VALIDATION
OF
THE
NUMERICAL
RESULTS
.
203
14.4.1
DRA
2303
AIRFOIL
.
203
14.4.2
MBB
VA
2
AIRFOIL
.
206
14.4.3
DA
LVA-1A
AIRFOIL
.
211
14.5
PARAMETRIC
STUDY
OF
THE
SC
DESIGN
PARAMETERS
.
214
14.5.1
POROSITY
.
214
14.5.2
PERFORATION
LOCATION
.
214
14.5.3
PERFORATION
LENGTH
.
217
14.6
CONCLUSION
.
217
14.7
REFERENCES
.
218
14.8
LIST
OF
SYMBOLS
.
219
15
DEVELOPMENT
OF
VISCOUS-INVISCID
INTERACTION
CODES
FOR
PREDICTION
OF
SHOCK
BOUNDARY-LAYER
INTERACTION
CONTROL
AND
BUFFET
OVER
AIRFOILS,
J.C.
LE
BALLEUR,
P.
GIRODROUX-LAVIGNE
AND
H.
GASSOT,
ONERA
.
221
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
15.1
INTRODUCTION
.
221
15.2
VISCOUS-INVISCID
INTERACTION
(VII)
NUMERICAL
METHODS
.
222
15.2.1
STEADY
CODE
VIS05C
(VII
+
FULL
POTENTIAL)
.
222
15.2.2
UNSTEADY
CODE
VIS15
(VII
+
TSP,
TIME-CONSISTENT
COUPLING)
.
223
15.2.3
SELF-ADAPTIVE
GRIDS
OF
CODES
VIS05
AND
VIS
15
.
223
15.3
SHOCK-CONTROL
EXTENSION
IN
CODES
VIS05CAND
VIS15
.
224
15.3.1
IMPLEMENTATION
OF
A
VELOCITY
AT
THE
WALL
.
224
15.3.2
CONTROL
LAWS
.
224
15.3.3
ISENTROPIC
LAW
.
225
15.3.4
POLL
'
S
FORMULA
.
225
15.3.5
ACTIVE
OR
PASSIVE
SHOCK-CONTROL
.
226
15.4
COMPUTATION
OF
STEADY
TEST-CASES
.
226
15.4.1
PRE-CALCULATIONS:
DA-LVA-1A
AIRFOIL
WITHOUT
CONTROL
.
226
15.4.2
DRA-2303
AIRFOIL
WITH/WITHOUT
CONTROL
.
228
15.4.3
VA2
AIRFOIL
WITH/WITHOUT
CONTROL
.
230
15.4.4
DA-LVA-L
A
AIRFOIL
WITH/WITHOUT
CONTROL
.
233
15.5
COMPUTATION
OF
THE
UNSTEADY
TEST-CASES
.
236
15.5.1
NLR7301
AIRFOIL
WITHOUT
CONTROL:
BUFFET
TEST-CASES
.
236
15.5.2
NACA0012
AIRFOIL
WITHOUT
CONTROL:
SEVERE
BUFFET
TEST-CASE
.
238
15.5.3
DRA-2303
AIRFOIL
WITH/WITHOUT
CONTROL:
DAMPING
OF
BUFFET
.
239
15.6
CONCLUSION
.
242
15.7
REFERENCES
.
243
16
TRANSONIC
AIRFOIL
FLOW
PREDICTION
WITH
SHOCK
BOUNDARY
LAYER
INTERACTION
CONTROL
BY
A
TIME-ACCURATE
NAVIER-STOKES
CODE,
W.
GEIBLER,
DLR
.
245
16.1
INTRODUCTION
.
245
16.2
NUMERICAL
METHOD
.
246
16.2.1
2D
TIME-ACCURATE
NAVIER-STOKES
CODE
.
246
16.2.2
IMPLEMENTATION
OF
SHOCK
CONTROL
LAWS
.
247
16.2.3
MODIFICATION
OF
TURBULENCE
MODEL
.
249
16.3
AIRFOILS
AND
TEST
CASES
.
250
16.4
RESULTS
.
251
16.4.1
STEADY
FLOW
.
251
16.4.2
UNSTEADY
FLOW,
BUFFET
.
252
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
16.5
FINAL
DISCUSSION
OF
RESULTS
.
253
16.5.1
STEADY
RESULTS
.
253
16.5.2
UNSTEADY
RESULTS
.
254
16.6
CONCLUSIONS
AND
FUTURE
ACTIVITIES
.
254
16.7
REFERENCES
.
255
17
SHOCK
BOUNDARY
LAYER
INTERACTION
CONTROL
PREDICTIONS
USING
A
VISCOUS-INVISCID
INTERACTION
PROCEDURE
AND
A
NAVIER-STOKES
SOLVER,
G.
SIMANDIRAKIS,
B.
BOURAS
AND
K.D.
PAPAILIOU,
UNIVERSITY
OF
ATHENS
.
265
17.1
INTRODUCTION
.
265
17.2
NUMERICAL
PROCEDURES
.
266
17.2.1
VISCOUS-INVISCID
INTERACTION
PROCEDURE
.
266
17.2.2
NAVIER-STOKES
APPROACH
.
271
17.2.3
SHOCK
CONTROL
LAWS
.
275
17.3
RESULTS
AND
DISCUSSION
.
277
17.3.1
VISCOUS-INVISCID
INTERACTION
RESULTS
.
277
17.3.2
NAVIER-STOKES
RESULTS
.
278
17.4
CONCLUSION
.
281
17.5
REFERENCES
.
281
18
COMPUTATION
OF
TRANSONIC
FLOWS
APPLYING
SHOCK
BOUNDARY
LAYER
INTERACTION
CONTROL,
B.A.
WOLLES,
NLR
.
291
18.1
INTRODUCTION
.
291
18.2
BASIC
PRINCIPLES
OF
PASSIVE
CONTROL
.
292
18.3
COMPUTATIONAL
METHOD
.
293
18.3.1
THE
ULTRAN-V
METHOD
.
293
18.3.2
EXTENSION
OF
ULTRA-V
TO
CONTROL
.
293
18.3.3
CONTROL
LAWS
.
294
18.3.4
IMPLEMENTATION
OF
THE
CONTROL
LAWS
.
296
18.4
NUMERICAL
RESULTS
.
296
18.4.1
STEADY
FLOW
PREDICTIONS
.
296
18.4.2
UNSTEADY
FLOW
PREDICTIONS
.
300
18.5
CONCLUSIONS
.
301
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
18.6
ACKNOWLEDGMENT
.
302
18.7
REFERENCES
.
302
19
DESIGN
AND
MANUFACTURE
OF
THE
CRYOGENIC
LAMINAR-TYPE
AIRFOIL
DA
LVA-1A
WITH
PASSIVE
SHOCK
CONTROL,
P.
THIEDE
AND
G.
DARGEL,
DAIMLER-BENZ
AEROSPACE
AIRBUS
GMBH
.
319
19.1
INTRODUCTION
.
319
19.2
BASIC
AIRFOIL
DA
LVA-1A
CHARACTERISTICS
.
319
19.2.1
AIRFOIL
DESIGN
.
319
19.2.2
REFERENCE
MEASUREMENTS
WITHOUT
SHOCK
CONTROL
.
321
19.3
CRYOGENIC
MODEL
DESIGN
I
MANUFACTURE
.
321
19.3.1
ONERA-T2
/
DLR-KRG
REQUIREMENTS
.
321
19.3.2
MODEL
CONSTRUCTION
I
MANUFACTURE
.
322
19.3.3
MODEL
EQUIPMENT
.
322
19.4
DESIGN
/
MANUFACTURE
OF
THE
PASSIVE
SHOCK
CONTROL
INSERTS
.
323
19.4.1
AERODYNAMIC
INSERT
DESIGN
PARAMETERS
.
323
19.4.2
INSERT
CONSTRUCTION
/MANUFACTURE/
EQUIPMENT
.
323
19.4.3
PERFORATION
TECHNIQUE
/
CHECK
OUT
PROCEDURE
.
325
19.4.4
ACTUAL
INSERT
PERFORATION
/
CALIBRATION
TESTS
.
325
19.5
CONCLUSIONS
.
329
19.6
REFERENCES
.
329
20
QUALIFICATION
BY
LASER
MEASUREMENTS
OF
THE
PASSIVE
CONTROL
ON
THE
LVA-1
A
AIRFOIL
IN
THE
T2
WIND
TUNNEL,
J.P.
ARCHAMBAUD
AND
A.M.
RODDE,
ONERA
/
CERT
.
331
20.1
INTRODUCTION
.
331
20.2
EXPERIMENTAL
SET-UP
AND
MEASUREMENT
CHARACTERISTICS
.
332
20.2.1
THE
T2
WIND
TUNNEL
.
332
20.2.2
LVA-LAE
MODEL
.
332
20.3
MEASUREMENTS
.
334
20.4
TEST
CONDITIONS
.
335
20.5
EXPERIMENTAL
DATA
.
336
20.5.1
DETERMINATION
OF
THE
NOMINAL
MACH
NUMBER
.
336
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
20.5.2
INCIDENCE
VARIATION
AT
M
=
0.77
.
336
20.5.3
LASER
MEASUREMENTS
.
342
20.6
CONCLUSIONS
.
351
20.7
TABLE
OF
RESULTS
.
352
20.8
LIST
OF
SYMBOLS
.
352
20.9
REFERENCES
.
353
21
EXPERIMENTAL
INVESTIGATION
OF
THE
TRANSONIC
AIRFOILS
DA
LVA-1A
AND
VA-2
WITH
SHOCK
CONTROL,
H.
ROSEMANN,
A.
KNAUER
AND
E.
STANEWSKY,
DLR
.
355
21.1
INTRODUCTION
.
355
21.2
INVESTIGATION
OF
THE
LAMINAR-TYPE
AIRFOIL
DA
LVA-LAE
WITHPASSIVE
CONTROL
AT
REYNOLDS
NUMBERS
OF
4.6
X
10
6
S
RE
S
12
X
10
6
.
357
21.2.1
THE
CRYOGENIC
LUDWIEG-TUBE
.
357
21.2.2
MODEL
AND
TEST
CONDITIONS
.
357
21.2.3
EXPERIMENTAL
RESULTS
.
358
21.3
INVESTIGATION
OF
THE
TURBULENT
AIRFOIL
VA-2
WITH
PASSIVE
AND
ACTIVE
CONTROL
.
366
21.3.1
VA-2
AIRFOIL
MODEL
AND
INSTRUMENTATION
.
366
21.3.2
WINDTUNNEL
.
367
21.3.3
TEST
CONDITIONS
.
367
21.3.4
ANALYSIS
AND
DISCUSSION
OF
RESULTS
.
368
21.4
CONCLUSIONS
.
377
21.5
NOMENCLATURE
.
378
21.6
REFERENCES
.
378
22
AN
EXPERIMENTAL
INVESTIGATION
OF
PASSIVE
SHOCK/BOUNDARY-LAYER
CONTROL
ON
AN
AEROFOIL,
J.L.
FULKER
AND
M.J.
SIMMONS,
DERA
.
379
22.1
INTRODUCTION
.
379
22.2
MODEL
DETAILS
AND
MEASUREMENTS
.
380
22.2.1
THE
MODEL
.
380
22.2.2
MEASUREMENTS
.
381
22.2.3
BOUNDARY-LAYER
TRANSITION
TRIPS
.
381
TABLE
OF
CONTENTS
(CONTINUED)
PAGE
22.2.4
TEST
CONDITIONS
.
381
22.3
EXPERIMENTAL
DATA
.
382
22.4
DISCUSSION
.
383
22.5
CONCLUSIONS
.
384
22.6
REFERENCES
.
385
22.7
LIST
OF
SYMBOLS
.
386
23
AN
EXPERIMENTAL
INVESTIGATION
OF
PASSIVE
SHOCK/BOUNDARY
LAYER
INTERACTION
CONTROL
ON
AN
AIRFOIL:
UNSTEADY
MEASUREMENTS,
W.
WAGNER,
DLR
.
401
23.1
INTRODUCTION
.
401
23.2
MEASUREMENTS
.
401
23.3
DATA
ACQUISITION
AND
INSTRUMENTATION
.
402
23.4
EXPERIMENTAL
RESULTS
.
402
23.5
REFERENCES
.
403
23.6
LIST
OF
SYMBOLS
.
404 |
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| classification_tum | MTA 450f MTA 420f MTA 425f |
| ctrlnum | (OCoLC)38316695 (DE-599)BVBBV011545670 |
| discipline | Physik |
| format | Book |
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| geographic | Europäische Union. Mitgliedsstaaten |
| geographic_facet | Europäische Union. Mitgliedsstaaten |
| id | DE-604.BV011545670 |
| illustrated | Illustrated |
| indexdate | 2024-08-18T00:08:49Z |
| institution | BVB |
| isbn | 3528076569 |
| language | German |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-007772889 |
| oclc_num | 38316695 |
| open_access_boolean | |
| owner | DE-91G DE-BY-TUM DE-210 DE-83 |
| owner_facet | DE-91G DE-BY-TUM DE-210 DE-83 |
| physical | 414 S. graph. Darst. 23 cm |
| publishDate | 1997 |
| publishDateSearch | 1997 |
| publishDateSort | 1997 |
| publisher | Vieweg |
| record_format | marc |
| series | Notes on numerical fluid mechanics |
| series2 | Notes on numerical fluid mechanics Community research in aeronautics |
| spelling | EUROSHOCK drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 ed. by Egon Stanewsky ... Braunschweig [u.a.] Vieweg 1997 414 S. graph. Darst. 23 cm txt rdacontent n rdamedia nc rdacarrier Notes on numerical fluid mechanics 56 Community research in aeronautics Literaturangaben Boundary layer control Research European Union countries Drag (Aeronautics) Research European Union countries Shock waves Research European Union countries Transonic planes Wings Design and construction Transonic planes Wings Research European Union countries Stoß-Grenzschicht-Wechselwirkung (DE-588)4282522-2 gnd rswk-swf Profilumströmung (DE-588)4175828-6 gnd rswk-swf Kompressible Strömung (DE-588)4032018-2 gnd rswk-swf Transsonische Strömung (DE-588)4135633-0 gnd rswk-swf Widerstandsverminderung (DE-588)4210098-7 gnd rswk-swf Viskose Strömung (DE-588)4226965-9 gnd rswk-swf Europäische Union. Mitgliedsstaaten Profilumströmung (DE-588)4175828-6 s Transsonische Strömung (DE-588)4135633-0 s Kompressible Strömung (DE-588)4032018-2 s Viskose Strömung (DE-588)4226965-9 s Stoß-Grenzschicht-Wechselwirkung (DE-588)4282522-2 s Widerstandsverminderung (DE-588)4210098-7 s DE-604 Stanewsky, Egon Sonstige oth Notes on numerical fluid mechanics 56 (DE-604)BV000898664 56 DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=007772889&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | EUROSHOCK drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 Notes on numerical fluid mechanics Boundary layer control Research European Union countries Drag (Aeronautics) Research European Union countries Shock waves Research European Union countries Transonic planes Wings Design and construction Transonic planes Wings Research European Union countries Stoß-Grenzschicht-Wechselwirkung (DE-588)4282522-2 gnd Profilumströmung (DE-588)4175828-6 gnd Kompressible Strömung (DE-588)4032018-2 gnd Transsonische Strömung (DE-588)4135633-0 gnd Widerstandsverminderung (DE-588)4210098-7 gnd Viskose Strömung (DE-588)4226965-9 gnd |
| subject_GND | (DE-588)4282522-2 (DE-588)4175828-6 (DE-588)4032018-2 (DE-588)4135633-0 (DE-588)4210098-7 (DE-588)4226965-9 |
| title | EUROSHOCK drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 |
| title_auth | EUROSHOCK drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 |
| title_exact_search | EUROSHOCK drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 |
| title_full | EUROSHOCK drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 ed. by Egon Stanewsky ... |
| title_fullStr | EUROSHOCK drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 ed. by Egon Stanewsky ... |
| title_full_unstemmed | EUROSHOCK drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 ed. by Egon Stanewsky ... |
| title_short | EUROSHOCK |
| title_sort | euroshock drag reduction by passive shock control results of the project euroshock aer2 ct92 0049 supported by the european union 1993 1995 |
| title_sub | drag reduction by passive shock control ; results of the project EUROSHOCK, AER2-CT92-0049 ; supported by the European Union, 1993 - 1995 |
| topic | Boundary layer control Research European Union countries Drag (Aeronautics) Research European Union countries Shock waves Research European Union countries Transonic planes Wings Design and construction Transonic planes Wings Research European Union countries Stoß-Grenzschicht-Wechselwirkung (DE-588)4282522-2 gnd Profilumströmung (DE-588)4175828-6 gnd Kompressible Strömung (DE-588)4032018-2 gnd Transsonische Strömung (DE-588)4135633-0 gnd Widerstandsverminderung (DE-588)4210098-7 gnd Viskose Strömung (DE-588)4226965-9 gnd |
| topic_facet | Boundary layer control Research European Union countries Drag (Aeronautics) Research European Union countries Shock waves Research European Union countries Transonic planes Wings Design and construction Transonic planes Wings Research European Union countries Stoß-Grenzschicht-Wechselwirkung Profilumströmung Kompressible Strömung Transsonische Strömung Widerstandsverminderung Viskose Strömung Europäische Union. Mitgliedsstaaten |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=007772889&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| volume_link | (DE-604)BV000898664 |
| work_keys_str_mv | AT stanewskyegon euroshockdragreductionbypassiveshockcontrolresultsoftheprojecteuroshockaer2ct920049supportedbytheeuropeanunion19931995 |