The characterisation & modification of wakes from lifting vehicles in fluids: papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996
Gespeichert in:
| Format: | Buch |
|---|---|
| Sprache: | English French |
| Veröffentlicht: |
Neuilly-sur-Seine
AGARD
1996
|
| Schriftenreihe: | AGARD conference proceedings
584 |
| Schlagworte: | |
| Online-Zugang: | Inhaltsverzeichnis |
| Beschreibung: | Literaturangaben |
| Beschreibung: | Getr. Zählung graph. Darst. |
| ISBN: | 9283600347 |
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| adam_text | AGARD-CP-584 ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 7 RUE
ANCELLE, 92200 NEUILLY-SUR-SEINE, FRANCE CONFERENCE PROCEEDINGS 584 THE
CHARACTERISATION & MODIFICATION OF WAKES FROM LIFTING VEHICLES IN FLUIDS
(LA CARACTERISATION ET LA MODIFICATION DES SILLAGES CREES DANS LES
FLUIDES PAR DES VEHICULES PORTANT) PAPERS PRESENTED AT THE FLUID
DYNAMICS PANEL SYMPOSIUM HELD IN TRONDHEIM, NORWAY, FROM 20-23 MAY 1996.
/~ NORTH ATLANTIC TREATY ORGANIZATION ORGANISATION DU TRAITE DE
L ATLANTIQUE NORD UNIVERSITATSBIBUOTHEK HANNOVER 1 TECHNISCHE
1NFORMATIONSBIBLIOTHEK ! UB/TIB HANNOVER 89 115 364 196 CONTENTS
EXECUTIVE SUMMARY SYNTHESE RECENT PUBLICATIONS OF THE FLUID DYNAMICS
PANEL FLUID DYNAMICS PANEL TECHNICAL EVALUATION REPORT BY W.J. MCCROSKEY
KEYNOTE SESSION CHAIRMAN: G.E.A. MEIER VORTEX WAKES IN AERODYNAMICS BY
H.W.M. HOEIJMAKERS WAKE VORTICES EFFECTS AND THE NEED FOR PROMPT ACTION
*A U.S. VIEW BY G.R. MACK WAKE VORTICES *A EUROPEAN REGULATORY VIEW BY
K. KOPLIN AIR TRAFFIC CONTROL PROCEDURES FOR THE AVOIDANCE OFWAKE VORTEX
ENCOUNTERS TODAY AND FUTURE DEVELOPMENTS BY DEUTSCHE FLUGSICHERUNG GMBH
BY F. BRENNER STRUCTURE OF A TRANSPORT AIRCRAFT-TYPE NEAR FIELD WAKE BY
K. HUENECKE THE INTERACTION BETWEEN AN INJECTED VORTEX AND A ROLLING UP
VORTEX SHEET BY M.R. DHANAK AND K.S. VISHWANTHAN FLOWFIELD PREDICTION OF
THREE-DIMENSIONAL WING TRAILING VORTICES USING ADVANCED TURBULENCE
MODELS BY J.A. EATON AND M.P. O FLAHERTY AN UNSTEADY VORTEX WAKE MODEL
FOR MANEUVERING VEHICLES BY M.R. MENDENHALL AND S.C. PERKINS, JR.
EXPERIMENTAL ASSESSMENT OF THE EXTENDED BETZ METHOD FOR WAKE VORTEX
PREDICTION X BY W.R. GRAHAM STRUCTURE, TRAJECTORY AND STRENGTH OFB747
AIRCRAFTWAKE VORTICES MEASUREDBY LASER BY J.M. VAUGHAN, D.W. BROWN, G.
CONSTANT, J.R. EACOCK AND R. FOORD PAGE III IV VIII X REFERENCE T 10 V
WAKE VORTEX DECAY NEAR THE GROUND UNDER CONDITIONS OF STRONG
STRATIFICATION AND WIND 11 SHEAR BY R.P. RUDIS, D.C, BURNHAM AND P.
JANOTA WAKE TURBULENCE TRAINING AND REGULATION: AN INDUSTRY TEAM
APPROACH 12 BY D.C. CARBAUGH AND W.D. FORSYTHE GROUND-BASED ANEMOMETER
MEASUREMENTS OFWAKE VORTICES FROM LANDING AIRCRAFT AT 13 AIRPORTS BY S.
ABRAMSON AND D.C. BURNHAM THE DYNAMIC RESPONSE OF A TWIN-ENGINE,
COMMERCIAL JET TRANSPORT TOWAKE VORTEX 14 ENCOUNTERS BY J. VASALKA
EXPERIMENTAL ANALYSIS OF THE VORTEX WAKE STRUCTURE BEHIND A
PROPELLER-WING CONFIGURATION 15 BY L.L.M. VELDHULS AND D.W.E. RENTEMA
FLOWFICLD OF A WING EMBEDDED IN THE WAKE OF A BURSTED VORTEX 16 BY
J.M.A. LONGO, M. ORLOWSKI AND D. STROHMEYER STABILITY OF MULTIPLE
TRAILING-VORTEX PAIRS 17 BY J.D. CROUCH INITIATION OF THE CROW
INSTABILITY BY ATMOSPHERIC TURBULENCE 18 BY P.R. SPALART AND A.A. WRAY
SIMULATION NUMERIQUE DIRECTE DE PINSTABILITE SINUSOIDALE 19 BY D. SIPP,
L. JACQUIN AND P. SAGAUT STABILITY THEORY FOR TWO WINGTIP VORTICES
BEHIND CRUISING AIRCRAFT 20 BY T. EHRET ANALYSIS OF UK ENCOUNTERS
1982-1990 21 BY D.C. BURNHAM A SIMULATION-BASED STUDY OF THE IMPACT OF
AIRCRAFT WAKE TURBULENCE WEIGHT CATEGORIES ON 22 AIRPORT CAPACITY BY
J.J. ROBINSON AN AIRCRAFT VORTEX SPACING SYSTEM (AVOSS) FOR DYNAMICAL
WAKE VORTEX SPACING CRITERIA 23 BY D.A. I-IINTON ON THE INTERACTION
BETWEEN TOPOGRAPHICALWIND AND LANDING AIRCRAFT 24 BY N. KUBBERUD, I. 0YE
AND H. N0RSTRUD FLOW FIELD SURVEY IN TRAILING VORTEX SYSTEM BEHIND A
CIVIL AIRCRAFT MODEL AT HIGH LIFT 25 BY A.C. DE BRUIN, S.H. HEGEN, P.B.
ROHNE AND P.R. SPALART MEASUREMENTS IN VORTEXWAKES SHED BY CONVENTIONAL
AND MODIFIED SUBSONIC AIRCRAFT 26 BY V.J. ROSSOW NATURAL AND FORCED
GROWTH CHARACTERISTICS OF THE VORTEX WAKE OF A RECTANGULAR AIRFOIL 27 BY
J.D. JACOB, D. LIEPMANN AND O. SAVAS, THREE-DIMENSIONAL DIRECT NUMERICAL
SIMULATIONS OFWAKE VORTICES: 28 ATMOSPHERIC TURBULENCE EFFECTS AND
REBOUND WITH CROSSWIND BY A. CORJON, F. RISSO, A. STOESSEL AND T.
POINSOT CARACTERISATION ET MODELISATION DU SILLAGE D UN AVION A PARTIR
D ESSAIS EN VOL DE MAQUETTES 29 EN LABORATOIRE BY P. COTON DIRECT
NUMERICAL SIMULATION OF THE BREAKDOWN OF AIRCRAFTWAKE VORTICES 30 BY
S.C. RENNICH AND S.K. LELE THE INVISCID MOTION OF A VORTEX PAIR IN A
COMPRESSIBLE AND STRATIFIED ATMOSPHERE 31 BY R. STUFF EXPERIMENTAL AND
NUMERICAL RESULTS ON SPIRAL VORTEX BREAKDOWN 32 BY S.H. BACKSTEIN
COMPUTATIONAL AND EXPERIMENTAL INVESTIGATION OF THE WAKES SHED FROM
FLAPPING AIRFOILS 33 AND THEIRWAKE INTERFERENCE/IMPINGEMENT
CHARACTERISTICS BY CM. DOHRING, M.F. PLATZER, K.D. JONES AND I.H. TUNCER
RECENT LABORATORY AND NUMERICAL TRAILING VORTEX STUDIES 34 BY D.P.
DELISI, G.C. GREENE, R.E. ROBINS AND R. SINGH WAKE DYNAMICSAND EXHAUST
DISTRIBUTION BEHIND CRUISING AIRCRAFT 35 BY T. GERZ AND T. EHRET THE USE
OFAIRCRAFT WAKES TO ACHIEVE POWER REDUCTIONS IN FORMATION FLIGHT 36 BY
D. HUMMEL ON THE DYNAMICS OFENGINE JETS BEHIND A TRANSPORT AIRCRAFT 37
BY L. JACQUIN AND F. GAMIER GENERAL DISCUSSION GD VII
|
| adam_txt |
AGARD-CP-584 ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 7 RUE
ANCELLE, 92200 NEUILLY-SUR-SEINE, FRANCE CONFERENCE PROCEEDINGS 584 THE
CHARACTERISATION & MODIFICATION OF WAKES FROM LIFTING VEHICLES IN FLUIDS
(LA CARACTERISATION ET LA MODIFICATION DES SILLAGES CREES DANS LES
FLUIDES PAR DES VEHICULES PORTANT) PAPERS PRESENTED AT THE FLUID
DYNAMICS PANEL SYMPOSIUM HELD IN TRONDHEIM, NORWAY, FROM 20-23 MAY 1996.
/~ NORTH ATLANTIC TREATY ORGANIZATION ORGANISATION DU TRAITE DE
L'ATLANTIQUE NORD UNIVERSITATSBIBUOTHEK HANNOVER 1 TECHNISCHE
1NFORMATIONSBIBLIOTHEK ! UB/TIB HANNOVER 89 115 364 196 CONTENTS
EXECUTIVE SUMMARY SYNTHESE RECENT PUBLICATIONS OF THE FLUID DYNAMICS
PANEL FLUID DYNAMICS PANEL TECHNICAL EVALUATION REPORT BY W.J. MCCROSKEY
KEYNOTE SESSION CHAIRMAN: G.E.A. MEIER VORTEX WAKES IN AERODYNAMICS BY
H.W.M. HOEIJMAKERS WAKE VORTICES' EFFECTS AND THE NEED FOR PROMPT ACTION
*A U.S. VIEW BY G.R. MACK WAKE VORTICES *A EUROPEAN REGULATORY VIEW BY
K. KOPLIN AIR TRAFFIC CONTROL PROCEDURES FOR THE AVOIDANCE OFWAKE VORTEX
ENCOUNTERS TODAY AND FUTURE DEVELOPMENTS BY DEUTSCHE FLUGSICHERUNG GMBH
BY F. BRENNER STRUCTURE OF A TRANSPORT AIRCRAFT-TYPE NEAR FIELD WAKE BY
K. HUENECKE THE INTERACTION BETWEEN AN INJECTED VORTEX AND A ROLLING UP
VORTEX SHEET BY M.R. DHANAK AND K.S. VISHWANTHAN FLOWFIELD PREDICTION OF
THREE-DIMENSIONAL WING TRAILING VORTICES USING ADVANCED TURBULENCE
MODELS BY J.A. EATON AND M.P. O'FLAHERTY AN UNSTEADY VORTEX WAKE MODEL
FOR MANEUVERING VEHICLES BY M.R. MENDENHALL AND S.C. PERKINS, JR.
EXPERIMENTAL ASSESSMENT OF THE EXTENDED BETZ METHOD FOR WAKE VORTEX
PREDICTION X BY W.R. GRAHAM STRUCTURE, TRAJECTORY AND STRENGTH OFB747
AIRCRAFTWAKE VORTICES MEASUREDBY LASER BY J.M. VAUGHAN, D.W. BROWN, G.
CONSTANT, J.R. EACOCK AND R. FOORD PAGE III IV VIII X REFERENCE T 10 V
WAKE VORTEX DECAY NEAR THE GROUND UNDER CONDITIONS OF STRONG
STRATIFICATION AND WIND 11 SHEAR BY R.P. RUDIS, D.C, BURNHAM AND P.
JANOTA WAKE TURBULENCE TRAINING AND REGULATION: AN INDUSTRY TEAM
APPROACH 12 BY D.C. CARBAUGH AND W.D. FORSYTHE GROUND-BASED ANEMOMETER
MEASUREMENTS OFWAKE VORTICES FROM LANDING AIRCRAFT AT 13 AIRPORTS BY S.
ABRAMSON AND D.C. BURNHAM THE DYNAMIC RESPONSE OF A TWIN-ENGINE,
COMMERCIAL JET TRANSPORT TOWAKE VORTEX 14 ENCOUNTERS BY J. VASALKA
EXPERIMENTAL ANALYSIS OF THE VORTEX WAKE STRUCTURE BEHIND A
PROPELLER-WING CONFIGURATION 15 BY L.L.M. VELDHULS AND D.W.E. RENTEMA
FLOWFICLD OF A WING EMBEDDED IN THE WAKE OF A BURSTED VORTEX 16 BY
J.M.A. LONGO, M. ORLOWSKI AND D. STROHMEYER STABILITY OF MULTIPLE
TRAILING-VORTEX PAIRS 17 BY J.D. CROUCH INITIATION OF THE CROW
INSTABILITY BY ATMOSPHERIC TURBULENCE 18 BY P.R. SPALART AND A.A. WRAY
SIMULATION NUMERIQUE DIRECTE DE PINSTABILITE SINUSOIDALE 19 BY D. SIPP,
L. JACQUIN AND P. SAGAUT STABILITY THEORY FOR TWO WINGTIP VORTICES
BEHIND CRUISING AIRCRAFT 20 BY T. EHRET ANALYSIS OF UK ENCOUNTERS
1982-1990 21 BY D.C. BURNHAM A SIMULATION-BASED STUDY OF THE IMPACT OF
AIRCRAFT WAKE TURBULENCE WEIGHT CATEGORIES ON 22 AIRPORT CAPACITY BY
J.J. ROBINSON AN AIRCRAFT VORTEX SPACING SYSTEM (AVOSS) FOR DYNAMICAL
WAKE VORTEX SPACING CRITERIA 23 BY D.A. I-IINTON ON THE INTERACTION
BETWEEN TOPOGRAPHICALWIND AND LANDING AIRCRAFT 24 BY N. KUBBERUD, I. 0YE
AND H. N0RSTRUD FLOW FIELD SURVEY IN TRAILING VORTEX SYSTEM BEHIND A
CIVIL AIRCRAFT MODEL AT HIGH LIFT 25 BY A.C. DE BRUIN, S.H. HEGEN, P.B.
ROHNE AND P.R. SPALART MEASUREMENTS IN VORTEXWAKES SHED BY CONVENTIONAL
AND MODIFIED SUBSONIC AIRCRAFT 26 BY V.J. ROSSOW NATURAL AND FORCED
GROWTH CHARACTERISTICS OF THE VORTEX WAKE OF A RECTANGULAR AIRFOIL 27 BY
J.D. JACOB, D. LIEPMANN AND O. SAVAS, THREE-DIMENSIONAL DIRECT NUMERICAL
SIMULATIONS OFWAKE VORTICES: 28 ATMOSPHERIC TURBULENCE EFFECTS AND
REBOUND WITH CROSSWIND BY A. CORJON, F. RISSO, A. STOESSEL AND T.
POINSOT CARACTERISATION ET MODELISATION DU SILLAGE D'UN AVION A PARTIR
D'ESSAIS EN VOL DE MAQUETTES 29 EN LABORATOIRE BY P. COTON DIRECT
NUMERICAL SIMULATION OF THE BREAKDOWN OF AIRCRAFTWAKE VORTICES 30 BY
S.C. RENNICH AND S.K. LELE THE INVISCID MOTION OF A VORTEX PAIR IN A
COMPRESSIBLE AND STRATIFIED ATMOSPHERE 31 BY R. STUFF EXPERIMENTAL AND
NUMERICAL RESULTS ON SPIRAL VORTEX BREAKDOWN 32 BY S.H. BACKSTEIN
COMPUTATIONAL AND EXPERIMENTAL INVESTIGATION OF THE WAKES SHED FROM
FLAPPING AIRFOILS 33 AND THEIRWAKE INTERFERENCE/IMPINGEMENT
CHARACTERISTICS BY CM. DOHRING, M.F. PLATZER, K.D. JONES AND I.H. TUNCER
RECENT LABORATORY AND NUMERICAL TRAILING VORTEX STUDIES 34 BY D.P.
DELISI, G.C. GREENE, R.E. ROBINS AND R. SINGH WAKE DYNAMICSAND EXHAUST
DISTRIBUTION BEHIND CRUISING AIRCRAFT 35 BY T. GERZ AND T. EHRET THE USE
OFAIRCRAFT WAKES TO ACHIEVE POWER REDUCTIONS IN FORMATION FLIGHT 36 BY
D. HUMMEL ON THE DYNAMICS OFENGINE JETS BEHIND A TRANSPORT AIRCRAFT 37
BY L. JACQUIN AND F. GAMIER GENERAL DISCUSSION GD VII |
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| spelling | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 The characterisation and modification of wakes from lifting vehicles in fluids Neuilly-sur-Seine AGARD 1996 Getr. Zählung graph. Darst. txt rdacontent n rdamedia nc rdacarrier AGARD conference proceedings 584 Literaturangaben Luftfahrttechnik (DE-588)4168244-0 gnd rswk-swf (DE-588)1071861417 Konferenzschrift gnd-content Luftfahrttechnik (DE-588)4168244-0 s DE-604 NATO Advisory Group for Aerospace Research and Development Sonstige (DE-588)378-5 oth AGARD conference proceedings 584 (DE-604)BV001900884 GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015344719&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
| spellingShingle | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 AGARD conference proceedings Luftfahrttechnik (DE-588)4168244-0 gnd |
| subject_GND | (DE-588)4168244-0 (DE-588)1071861417 |
| title | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 |
| title_alt | The characterisation and modification of wakes from lifting vehicles in fluids |
| title_auth | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 |
| title_exact_search | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 |
| title_exact_search_txtP | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 |
| title_full | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 |
| title_fullStr | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 |
| title_full_unstemmed | The characterisation & modification of wakes from lifting vehicles in fluids papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 |
| title_short | The characterisation & modification of wakes from lifting vehicles in fluids |
| title_sort | the characterisation modification of wakes from lifting vehicles in fluids papers presented at the fluid dynamcis panel symposium held in trondheim norway from 20 23 may 1996 |
| title_sub | papers presented at the Fluid Dynamcis panel Symposium held in Trondheim, Norway, from 20-23 May 1996 |
| topic | Luftfahrttechnik (DE-588)4168244-0 gnd |
| topic_facet | Luftfahrttechnik Konferenzschrift |
| url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015344719&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
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