Second International Symposium on Aeroelasticity and Structural Dynamics: collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985
Saved in:
| Corporate Author: | |
|---|---|
| Format: | Conference Proceeding Book |
| Language: | English |
| Published: |
Bonn
Dt. Ges. für Luft- und Raumfahrt, (DGLR)
1985
|
| Series: | Deutsche Gesellschaft für Luft- und Raumfahrt: DGLR-Bericht.
85,2 |
| Subjects: | |
| Online Access: | Inhaltsverzeichnis |
| Item Description: | Literaturangaben |
| Physical Description: | VII, 699 S. graph. Darst. |
| ISBN: | 3922010288 |
Staff View
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| 245 | 1 | 0 | |a Second International Symposium on Aeroelasticity and Structural Dynamics |b collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 |c International Symposium on Aeroelasticity and Structural Dynamics <2, 1985, Aachen> ; Deutsche Gesellschaft für Luft- und Raumfahrt* |
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Record in the Search Index
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| adam_text | IMAGE 1
DGLR-BERICHT 85-02
*$* DFVLR
SECOND
INTERNATIONAL SYMPOSIUM ON AEROELASTICITY AND
STRUCTURAL DYNAMICS
ONERA
COLLECTED PAPERS OFTHE SYMPOSIUM HELD IN AACHEN, W. GERMANY, APRIL
1-3,1985
ORGANIZED BY
DEUTSCHE GESELLSCHAFT FUR LUFT- UND RAUMFAHRT E.V. (DGLR), BONN, W.
GERMANY
IN COOPERATION WITH
DEUTSCHE FORSCHUNGS- UND VERSUCHSANSTALT FUR LUFT- UND RAUMFAHRT E.V.
(DFVLR-AVA), GOTTINGEN, W. GERMANY
NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM (NLR), AMSTERDAM, THE
NETHERLANDS
OFFICE NATIONAL D ETUDES ET DE RECHERCHES AEROSPATIALES (ONERA), PARIS,
FRANCE
DIE ERSTELLUNG DIESES BERICHTES WURDE VOM BUNDESMINISTER FUR FORSCHUNG
UND TECHNOLOGIE GEFORDERT. TIB/UB HANNOVER 89
IMAGE 2
CONTENTS
PAGE
ORGANIZING AND PROGRAM COMMITTEE
FOREWORD
SESSION I: UNSTEADY AERODYNAMICS AND AEROELASTIC CHARACTERISTICS
CHAIRMAN: B. LASCHKA,
TECHN. DNIV. BRAUNSCHWEIG/W. GERMANY
1. CALCULATION OF TRANSONIC STEADY AND OSCILLATORY PRESSURES ON A LOW
ASPECT RATIO MODEL AND COMPARISON WITH EXPERIMENT , 1
R.M. BENNETT AND E.C. WYNNE, NASA LANGLEY RES. CTR., HAMPTON, VA/USA AND
D.G. MABEY, RAE BEDFORD/UK
2. TRANSONIC EQUIVALENT STRIP METHOD FOR AEROELASTIC APPLICATIONS 17
D.D. LUI AND Y.F. KAO, ARIZ. STATE UNIVERSITY, TEMPE, AZ/USAAND K.Y.
FUNG, UNIV. OF ARIZONA, TUCSON, AZ/USA
3. CALCULATION OF 3-D UNSTEADY TRANSONIC POTENTIAL FLOWS BY A FIELD
PANEL METHOD 33
R. VOSS, DFVLR-AVA, GOTTINGEN/W.GERMANY
4. APPLICATION OF TRANSONIC UNSTEADY METHODS FOR CALCULATION OF FLUTTER
AIRLOADS 47
H. ZIMMERMANN AND S. VOGEL, MBB, BREMEN/W.GERMANY
5. EXTENSION AND USE OF A NUMERICAL PROCEDURE FOR THREE DIMENSIONAL
UNSTEADY TRANSONIC FLOWS . . 62
P. MULAK, J.L. MEURZEC AND J.J. ANGELINI, ONERA, CHATILLON/FRANCE
6. EXACT CLOSED-FORM SOLUTIONS FOR NONLINEAR UNSTEADY TRANSONIC
AERODYNAMICS 71
G.A. OYIBO, FAIRCHILD REP. CO., FARMINGDALE, NY/USA
CHAIRMAN: H. ZIMMERMANN
MBB, BREMEN/W.GERMANY
7. RECENT TRANSONIC UNSTEADY PRESSURE MEASUREMENTS AT THE NASA LANGLEY
RESEARCH CENTER ... 80 M.C. SANDFORD, R.H. RICKETTS AND R.W. HESS, NASA
LANGLEY RES. CTR., HAMPTON, VA/USA
8. STEADY AND UNSTEADY PRESSURE DISTRIBUTIONS ON VARIOUS PROFILES IN
SEPARATED SUBSONIC AND TRANSONIC FLOW 99
H. TRIEBSTEIN, DFVLR-AVA, G6TTINGEN/W .GERMANY
9. SOME RESULTS OF EXPERIMENTAL AND ANALYTICAL BUFFETING INVESTIGATIONS
ON A DELTA WING 120
J. BECKER, MBB, MUNICH/W.GERMANY AND A. GRAVELLE, ONERA,
CHATILLON/FRANCE
10. AN IMPROVED POTENTIAL GRADIENT METHOD FOR THE COMPUTATION OF
UNSTEADY AERODYNAMIC PRESSURES ON OSCILLATING WINGS IN SUPERSONIC FLOW
153
F.Q. ZHANG AND H. FORSCHING, DFVLR-AVA, GOTTINGEN/W.GERMANY
11. AN EXACT FORMULATION OF THE UNSTEADY AERODYNAMIC THEORY OF LIFTING
SURFACES UNDERGOING ARBITRARY SMALL MOTIONS IN A SUPERSONIC FLOW FIELD
163 L. LIBRESCU, TEL-AVIV UNIV., RAMAT AVIV/ISRAEL
12. THREE-DIMENSIONAL FULLY UNSTEADY AERODYNAMICS AND ITS APPLICATION TO
FLUTTER CALCULATIONS... Q. LIU, Y. YANG, NORTHWESTERN POLYTECHN. UNIV.,
XI AN/PR CHINA [PAPER WITHDRAWN]
III
IMAGE 3
SESSION I (CON T)
CHAIRMAN: H. FORSCHING,
DFVLR-AVA, GOTTINGEN/W .GERMANY
PAGE
13. THEORETICAL FLUTTER INVESTIGATIONS ON A PLANE CASCADE IN
INCOMPRESSIBLE FLOW 189
V. CARSTENS, DFVLR-AVA, GOTTINGEN/W .GERMANY
14. APPLICATION OF UNSTEADY WING COLLOCATION METHODS TO CASCADES IN
SUBSONIC FLOW 180
A. KLOSE AND B. LASCHKA, TECHN. UNIV. BRAUNSCHWEIG/W.GERMANY
15. A NUMERICAL ANALYSIS FOR VERTICAL GUST FIELD INDUCED BY GUST
GENERATOR 187
Y. YANG AND J. WANG, NORTHWESTERN POLYTECHN. UNIV., XI AN/PR CHINA
16. A NEW LOOK AT ARBITRARY MOTION UNSTEADY AERODYNAMICS AND ITS
APPLICATION TO ROTARY-WING AEROELASTICITY 194
P.P. FRIEDMANN, UCLA, LOS ANGELES, CA/USA
17. EXPERIMENTAL TRANSONIC PRESSURE DISTRIBUTIONS OF A FLEXIBLE
WING-AILERON MODEL AND COMPARISONS WITH RESULTS OF SEVERAL THEORETICAL
METHODS 211
D. GUAN, W. LIU, Z. GAO AND Y. ZHANG, SHENYANG AIRCRAFT CORP,
SHENYANG/PR CHINA
18. CALCULATION OF THE LOAD DISTRIBUTION, AERODYNAMIC DERIVATIVES AND
DYNAMIC CHARACTERISTICS OF QUASI-STATIC ELASTIC AIRCRAFT 219
Q. LIU, C. WU, Z. JIAN AND K. WU, NORTHWESTERN POLYTECHN. UNIV.,
XI AN/PR CHINA
CHAIRMAN: R. DAT,
ONERA, CHATILLON/FRANCE
19. STATIC AEROELASTIC ANALYSIS USING AIRCRAFT VIBRATION MODES 229
Z. SHEENA AND M. KARPEL, ISRAEL AIRCRAFT INDUSTRIES, BEN-GURION
AIRPORT/ISRAEL
20. A REVIEW OF AEROELASTIC RESEARCH AT THE FLIGHT DYNAMICS LABORATORY
233
T.M. HARRIS, T.E. NOLL, T.J. HERTZ AND W.A. SOTOMAYER, U.S. AIR FORCE
WRIGHT AERO NAUTICAL LABORATORIES
21. SELECTED TOPICS IN EXPERIMENTAL AEROELASTICITY AT THE NASA LANGLEY
RESEARCH CENTER 244 R.H. RICKETTS, NASA, WASHINGTON, DC/USA
22. AEROELASTIC WIND TUNNEL SIMILARITY THEORY FOR ANISOTROPIC AIRCRAFT
WINGS . 257
G.A. OYIBO, FAIRCHILD REPUBLIC CO., FARMINGDALE, NY/USA
23. THE CHOICE OF TECHNIQUES USED FOR FLIGHT FLUTTER CLEARANCE WITH
PARTICULAR REFERENCE TO THE BAE 146 AND BAE 125 265
A.G. WOODS, BAE, HATFIELD/UK
24. FLUTTER CALCULATION BY A NEW PROGRAM 276
V.J.E. STARK, SAAB SCANIA AB, LINKOPING/SWEDEN
25. EXPERIENCE WITH AEROELASTIC ANALYSIS OF A SINGLE ENGINE TURBO
TRAINER USING FINITE ELEMENTS METHODS 286
M.J. REINICKE AND A.S. TURI, PILATUS AIRCRAFT LTD, STANS/SWITZERLAND AND
A. VOLLAN, OMERA GMBH, IMMENSTAAD/W.GERMANY
IV
IMAGE 4
SESSION II.L: ACTIVE CONTROL TECHNOLOGY
CHAIRMAN: H. HONLINGER, MBB, MUNICH/W.GERMANY
PAGE
26. DEVELOPMENT OF A FLUTTER SUPRESSION CONTROL LAW BY USE OF LINEAR
QUADRATIC GAUSSIAN AND CONSTRAINED OPTIMIZATION DESIGN TECHNIQUES 297
W.M. ADAMS, JR. AND S.H. TIFFANY, NASA LANGLEY RES. CTR., HAMPTON,
VA/USA 27. FINITE STATE MODELLING OF AEROELASTIC SYSTEMS FOR ACTIVE
CONTROL APPLICATIONS: A GENERAL THEORY 309 R. VEPA, QUEEN MARY COLLEGE,
LONDON/UK
28. NLR EXPERIENCE IN THE APPLICATION OF ACTIVE FLUTTER SUPPRESSION AND
GUST LOAD ALLEVIATION, APPLIED TO A WIND-TUNNEL MODEL 320
P. A. VAN GELDER, NLR, AMSTERDAM/THE NETHERLANDS
29. THE DESIGN AND WIND TUNNEL DEMONSTRATION OF AN ACTIVE CONTROL SYSTEM
FOR GUST LOAD ALLEVIATION AND FLUTTER SUPPRESSION 330
I.W. KAYNES, C.W. SKINGLE AND J.C. COPLEY, RAE, FARNBOROUGH/UK
30. ACTIVE CONTROL OF THE BUFFETING RESPONSE ON A LARGE MODERN CIVIL
AIRPLANE CONFIGURATION IN WIND TUNNEL 348
R. DESTUYNDER, ONERA, CHATILLON/FRANCE
31. WINDTUNNEL TEST AND LABORATORY SIMULATION OF A LOAD ALLEVIATION
SYSTEM FOR A MODERN TRANS PORT AIRCRAFT 356
H.G. GIEBELER AND G. BEUCK, MBB, HAMBURG/W.GERMANY
32. CONTROL LAW SYNTHESIS FOR GUST LOAD ALLEVIATION USING LINEAR
QUADRATIC GAUSSIAN THEORY ... 362 J. CHANG, NORTHWESTERN POLYTECHN.
UNIV., XI AN/PR CHINA
33. STIFFNESS CONTROL OF LARGE SPACE STRUCTURES 367
J.-C. CHEN AND J.L. FANSON, CALIF. INST, OF TECHNOLOGY, PASADENA, CA/USA
34. ASPECTS OF ACTIVE ISOLATION AS APPLIED TO A SATELLITE STRUCTURE WITH
SHAPE PRECISION PAYLOAD . . 374 W. CHARON, DORNIER SYSTEM,
FRIEDRICHSHAFEN/W.GERMANY
R
SESSION II.2: STRUCTURAL MODELLING AND OPTIMIZATION
CHAIRMAN: 0. SENSBURG,
MBB, MUNICH/W.GERMANY
35. THE APPLICATION OF PRACTICAL OPTIMIZATION TECHNIQUES IN THE
PRELIMINARY STRUCTURAL DESIGN OF A FORWARD-SWEPT WING 381
E. LERNER, GRUMMAN AEROSPACE CORP., BETHPAGE, NY/USA
36. STRUCTURAL OPTIMISATION PROGRAMS AND METHODS 393
A.J. MORRIS, CRANFIELD INSTITUTE OF TECHN., BEDFORD/UK
37. VARIATION OF ANISOTROPIC BEHAVIOUR IN STRUCTURAL OPTIMIZATION 407
G. HORNUNG, D.W. MATHIAS AND H. ROHRLE, DORNIER GMBH,
FRIEDRICHSHAFEN/W.GERMANY
38. TAILORING METHODOLOGY FOR AEROELASTIC STABILITY AND LATERAL CONTROL
ENHANCEMENT 415 T.A. WEISSHAAR, PURDUE UNIV., W. LAFAYETTE, IN/USA
39. STRUCTURAL OPTIMIZATION WITH CONSTRAINTS IN DYNAMICS
426
H.J. BAIER, DORNIER SYSTEM GMBH, FRIEDRICHSHAFEN/W.GERMANY
40. ANISOTROPIC WING AEROELASTIC THEORIES WITH WARPING EFFECTS 434
G.A. OYIBO AND J.H. BERMAN, FAIRCHILD REPUBLIC CO., FARMINGDALE, NY/USA
41. RECENT RESULTS ON THE WEIGHT MINIMIZATION OF PANELS WITH A FLUTTER
SPEED CONSTRAINT 441 L. LIBRESCU AND L. BEINER, TEL-AVIV UNIVERSITY,
RAMAT AVIV/ISRAEL
42. EFFECTS OF ANISOTROPIC DESIGN ON THE STATIC AEROELASTICITY OF A
SWEPT WING 451
M. PIENING, DFVLR, BRAUNSCHWEIG/W.GERMANY
V
IMAGE 5
SESSION II.2 (CON T)
CHAIRMAN: R.J. ZWAAN,
NLR, AMSTERDAM/THE NETHERLANDS
PAGE
43. AEROELASTIC PROBLEMS AND STRUCTURAL DESIGN OF A TAILLESS
CFC-SAILPLANE 457
J. SCHWEIGER AND O. SENSBURG, MBB, MUNICH/W.GERMANY AND
H.J. BERNS, TECHN. UNIV. BRAUNSCHWEIG/W.GERMANY
44. SIMULATION OF AIRCRAFT TAXI TESTING ON THE AGILE SHAKER TEST
FACILITY 468
R. FREYMANN, DFVLR-AVA, GOTTINGEN/W.GERMANY AND W.P. JOHNSON,
WRIGHT-PATTERSON AIR FORCE BASE, DAYTON, OH/USA
45. DYNAMIC ANALYSIS OF STRUCTURES WITH FLEXIBLE ROTORS 477
M. GERADIN AND N. KILL, UNIV. OF LIEGE/BELGIUM
46. STRUCTURAL DYNAMIC ASPECTS OF ROTOR NODAL ISOLATION 486
J. STOPPEL, MBB, MUNICH/W.GERMANY
47. ANALYTICAL FINITE ELEMENTS 495
P.H. KULLA, RESSULT, S6CHTENAU/W.GERMANY
48. INFLUENCE OF AXIAL FORCE ON RANDOM VIBRATION RESPONSE OF A STRUCTURE
504
I. ELISHAKOFF, TECHNION, HAIFA/ISRAEL
SESSION HI. 1: STRUCTURAL SYSTEM IDENTIFICATION
CHAIRMAN: E. BREITBACH,
DFVLR-AVA, GOTTINGEN/W.GERMANY
49. DETERMINATION OF BOTH COMPLEX CHARACTERISTIC STRUCTURAL VALUES AND
NORMAL MODE PARAMETERS FROM
HARMONIC EXCITATION NEAR RESONANCE 512
J. ARTMANN, DORNIER GMBH, FRIEDRICHSHAFEN/W.GERMANY
50. ADVANCES IN GROUND VIBRATION TESTING USING A COMBINATION OF PHASE
RESONANCE AND PHASE SEPARATION METHODS 523 N. NIEDBAL, DFVLR-AVA,
GOTTINGEN/W. GERMANY
51. SIMULTANEOUS DETERMINATION OF NORMAL EIGENMODES AND GENERALIZED
DAMPING MATRIX FROM COMPLEX
EIGENMODES 529
Q. ZHANG AND G. LALLEMENT, UNIV. DE FRANCHE-COMTE, BESANCON/FRANCE
52. IDENTIFICATION AND DYNAMIC CONDENSATION OF PHYSICAL SYSTEM MATRICES
USING INCOMPLETE DYNAMIC RESPONSE DATA 536
M. LINK AND K. BADENHAUSEN, UNIV. OF KASSEL/W.GERMANY
53. MODAL PARAMETER ESTIMATION FROM DRIVEN-BASE TESTS 546
S. DRAISEY, SPAR AEROSPACE LTD., TORONTO/CANADA AND F.R. VIGNERON AND Y.
SOUCY, DEPT. OF COMMUNICATIONS, OTTAWA/CANADA AND J.-G. BELIVEAU, UNIV.
DE SHERBROOKE/CANADA
54. DETERMINATION OF FORCE DISTRIBUTIONS IN MULTI-POINT RESONANCE
TESTING USING VARIOUS DIRECT METHODS 553
K. ALEXIOU AND J.R. WRIGHT, QUEEN MARY COLLEGE, LONDON/UK
CHAIRMAN: M. LINK,
UNIV. OF KASSEL/W.GERMANY
55. EIGENSOLUTIONS IDENTIFICATION OF NON SELF-ADJOINT MECHANICAL
STRUCTURES 565
Q. ZHANG AND G. LALLEMENT, UNIV. DE FRANCHE-COMTE, BESANCON/FRANCE
VI
IMAGE 6
SESSION III.I (CON T)
PAGE
56. RECENT DEVELOPMENTS IN THE IDENTIFICATION OF NON-LINEARITY IN MODAL
TESTING 571
G.R. TOMLINSON, UNIV. OF MANCHESTER/UK
57. ADVANCES IN TIME DOMAIN MODAL IDENTIFICATION AND MODELING OF
STRUCTURES 581
S.R. IBRAHIM, OLD DOMINION UNIV., NORFOLK, VA/USA
58. COMPARISON OF SOME TIME DOMAIN METHODS FOR STRUCTURAL SYSTEM
IDENTIFICATION 595
J.E. COOPER AND J.R. WRIGHT, QUEEN MARY COLLEGE, LONDON/UK
59. DETERMINATION OF NATURAL VIBRATION PROPERTIES OF A WING WITH WINGLET
BY EXPERIMENTAL MODE SYNTHESIS TECHNIQUE 605
S.N. GU, W.J. YOU AND J.S. JIANG, NORTHWESTERN POLYTECHN. UNIV.,
XI AN/PR CHINA
60. RAPID VIBRATION MODE ANALYSIS OF AIRCRAFT WITH EXTERNAL STORES 612
M. KARPEL, ISRAEL AIRCRAFT INDUSTRIES, BEN-GURION AIRPORT/ISRAEL
CHAIRMAN: E. HORNUNG,
MBB-ERNO , BREMEN/W.GERMANY
61. ANALYSIS-TEST CORRELATION AND UPDATE OF DYNAMIC MATHEMATICAL MODELS
B. CAESAR, DORNIER SYSTEM, FRIEDRICHSHAFEN/W .GERMANY
62. UPDATING MATHEMATICAL MODELS ON THE BASIS OF VIBRATION AND MODAL
TEST RESULTS - A REVIEW OF EXPERIENCE . ,
H.G. NATKE AND N. COTTIN, UNIV. OF HANNOVER/W,GERMANY
63. TEST AND ANALYSIS CORRELATION FOR STRUCTURAL DYNAMIC SYSTEMS B.K.
WADA AND J.-C. CHEN, CALIF. INST, OF TECHN., PASADENA, CA/USA
SESSION HI.2: STRUCTURAL DYNAMICS DESIGN VERIFICATION OF SPACE
STRUCTURES
CHAIRMAN: E. HORNUNG,
MBB-ERNO, BREMEN/W.GERMANY
61. DYNAMIC VERIFICATION OF VERY LARGE SPACE STRUCTURES 648
B.R. HANKS, NASA LANGLEY RES. CTR., HAMPTON, VA/USA
62. RECONSTRUCTION OF FORCING FUNCTIONS BASED ON MEASURED STRUCTURAL
RESPONSES 656
H. DRY, H. GLASER AND D. HOLZDEPPE, TECHN. UNIV. OF AACHEN/W. GERMANY
CHAIRMAN: H. DRY,
TECHN. UNIV. OF AACHEN/W.GERMANY
63. SPACECRAFT STRUCTURES DESIGN AND VERIFICATION C. STAVRINIDIS, ESA,
NOORDWIJK/THE NETHERLANDS
64. LOW FREQUENCY DESIGN VERIFICATION OF LARGE SPACECRAFT STRUCTURES E.
ERBEN AND K. ECKHARDT, MBB-ERNO, BREMEN/W.GERMANY
65. VIBRATION QUALIFICATION AT THE DAVID FLORIDA LABORATORY R. MAMEN,
DAVID FLORIDA LAB. , OTTAWA/CANADA
66. INFLUENCE OF NONLINEAR SPACECRAFT COMPONENTS ON DYNAMIC LAUNCH AND
IN-ORBIT RESPONSE I. KOLSCH AND H. BAIER, DORNIER SYSTEM,
FRIEDRICHSHAFEN/W,GERMANY
67. SIGNIFICANCE AND RELIABILITY OF DYNAMIC ANALYSIS METHODS
DEMONSTRATED IN THE INSTRUMENT POINTING SYSTEM PROJECT E. HILBRANDT AND
J.H. KROKER, DORNIER SYSTEM, FRIEDRICHSHAFEN/W .GERMANY
VII
617
625
632
669
672
683
689
697
|
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| genre | (DE-588)1071861417 Konferenzschrift 1985 Aachen gnd-content |
| genre_facet | Konferenzschrift 1985 Aachen |
| id | DE-604.BV002051126 |
| illustrated | Illustrated |
| indexdate | 2024-07-09T15:39:30Z |
| institution | BVB |
| institution_GND | (DE-588)16169950-9 (DE-588)6840-8 |
| isbn | 3922010288 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-001341253 |
| oclc_num | 16760095 |
| open_access_boolean | |
| owner | DE-91 DE-BY-TUM |
| owner_facet | DE-91 DE-BY-TUM |
| physical | VII, 699 S. graph. Darst. |
| publishDate | 1985 |
| publishDateSearch | 1985 |
| publishDateSort | 1985 |
| publisher | Dt. Ges. für Luft- und Raumfahrt, (DGLR) |
| record_format | marc |
| series | Deutsche Gesellschaft für Luft- und Raumfahrt: DGLR-Bericht. |
| series2 | Deutsche Gesellschaft für Luft- und Raumfahrt: DGLR-Bericht. |
| spelling | International Symposium on Aeroelasticity and Structural Dynamics 2 1985 Aachen Verfasser (DE-588)16169950-9 aut Second International Symposium on Aeroelasticity and Structural Dynamics collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 International Symposium on Aeroelasticity and Structural Dynamics <2, 1985, Aachen> ; Deutsche Gesellschaft für Luft- und Raumfahrt* Bonn Dt. Ges. für Luft- und Raumfahrt, (DGLR) 1985 VII, 699 S. graph. Darst. txt rdacontent n rdamedia nc rdacarrier Deutsche Gesellschaft für Luft- und Raumfahrt: DGLR-Bericht. 85,2 Literaturangaben Aerodynamics Congresses Aeroelasticity Congresses Aerodynamik (DE-588)4000589-6 gnd rswk-swf Aeroelastizität (DE-588)4202469-9 gnd rswk-swf Raumfahrzeug (DE-588)4048579-1 gnd rswk-swf Strukturdynamik (DE-588)4226174-0 gnd rswk-swf (DE-588)1071861417 Konferenzschrift 1985 Aachen gnd-content Strukturdynamik (DE-588)4226174-0 s Raumfahrzeug (DE-588)4048579-1 s DE-604 Aerodynamik (DE-588)4000589-6 s Aeroelastizität (DE-588)4202469-9 s Deutsche Gesellschaft für Luft- und Raumfahrt Sonstige (DE-588)6840-8 oth Deutsche Gesellschaft für Luft- und Raumfahrt: DGLR-Bericht. 85,2 (DE-604)BV000785535 85,2 GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=001341253&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | Second International Symposium on Aeroelasticity and Structural Dynamics collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 Deutsche Gesellschaft für Luft- und Raumfahrt: DGLR-Bericht. Aerodynamics Congresses Aeroelasticity Congresses Aerodynamik (DE-588)4000589-6 gnd Aeroelastizität (DE-588)4202469-9 gnd Raumfahrzeug (DE-588)4048579-1 gnd Strukturdynamik (DE-588)4226174-0 gnd |
| subject_GND | (DE-588)4000589-6 (DE-588)4202469-9 (DE-588)4048579-1 (DE-588)4226174-0 (DE-588)1071861417 |
| title | Second International Symposium on Aeroelasticity and Structural Dynamics collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 |
| title_auth | Second International Symposium on Aeroelasticity and Structural Dynamics collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 |
| title_exact_search | Second International Symposium on Aeroelasticity and Structural Dynamics collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 |
| title_full | Second International Symposium on Aeroelasticity and Structural Dynamics collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 International Symposium on Aeroelasticity and Structural Dynamics <2, 1985, Aachen> ; Deutsche Gesellschaft für Luft- und Raumfahrt* |
| title_fullStr | Second International Symposium on Aeroelasticity and Structural Dynamics collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 International Symposium on Aeroelasticity and Structural Dynamics <2, 1985, Aachen> ; Deutsche Gesellschaft für Luft- und Raumfahrt* |
| title_full_unstemmed | Second International Symposium on Aeroelasticity and Structural Dynamics collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 International Symposium on Aeroelasticity and Structural Dynamics <2, 1985, Aachen> ; Deutsche Gesellschaft für Luft- und Raumfahrt* |
| title_short | Second International Symposium on Aeroelasticity and Structural Dynamics |
| title_sort | second international symposium on aeroelasticity and structural dynamics collected papers of the symposium held in aachen w germany april 1 3 1985 |
| title_sub | collected papers of the symposium held in Aachen, W. Germany, April 1 - 3, 1985 |
| topic | Aerodynamics Congresses Aeroelasticity Congresses Aerodynamik (DE-588)4000589-6 gnd Aeroelastizität (DE-588)4202469-9 gnd Raumfahrzeug (DE-588)4048579-1 gnd Strukturdynamik (DE-588)4226174-0 gnd |
| topic_facet | Aerodynamics Congresses Aeroelasticity Congresses Aerodynamik Aeroelastizität Raumfahrzeug Strukturdynamik Konferenzschrift 1985 Aachen |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=001341253&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
| volume_link | (DE-604)BV000785535 |
| work_keys_str_mv | AT internationalsymposiumonaeroelasticityandstructuraldynamicsaachen secondinternationalsymposiumonaeroelasticityandstructuraldynamicscollectedpapersofthesymposiumheldinaachenwgermanyapril131985 AT deutschegesellschaftfurluftundraumfahrt secondinternationalsymposiumonaeroelasticityandstructuraldynamicscollectedpapersofthesymposiumheldinaachenwgermanyapril131985 |