Advances in rotorcraft technology: papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996
Gespeichert in:
Format: | Buch |
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Sprache: | English |
Veröffentlicht: |
Neuilly-sur-Seine
AGARD
1997
|
Schriftenreihe: | AGARD conference proceedings
592 |
Schlagworte: | |
Online-Zugang: | Inhaltsverzeichnis |
Beschreibung: | Getr. Zählung |
ISBN: | 928360038X |
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adam_text | AGARD-CP-592 ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 7 RUE
ANCELLE, 92200 NEUILLY-SUR-SEINE, FRANCE AGARD CONFERENCE PROCEEDINGS
592 ADVANCES IN ROTORCRAFT TECHNOLOGY (LES AVANCEES EN TECHNOLOGIES POUR
AERONEFS A VOILURE TOURNANTE) PAPERS PRESENTED AT THE FLIGHT VEHICLE
INTEGRATION PANEL SYMPOSIUM HELD IN OTTAWA, CANADA, 27-30MAY 1996. NORTH
ATLANTIC TREATY ORGANIZATION ORGANISATION DU TRAITE DE L ATLANTIQUE NORD
UB/TIB HANNOVER 115 801 979 89 CONTENTS EXECUTIVE SUMMARY SYNTHESE
THEME/THEME FLIGHT VEHICLE INTEGRATION PANEL ACKNOWLEDGEMENTS TECHNICAL
EVALUATION REPORT BY M. SINCLAIR KEYNOTE ADDRESS 1 BY B.GEN. K.R. PENNIE
KEYNOTE ADDRESS 2 BY GEN. C. BATLLO CERTIFICATION OF MODEL 230
HELICOPTER FOR CATEGORY A ELEVATED HELIPAD OPERATIONS BY J. GOLDENBERG,
L. MESLIN, M. BLONDINO AND D. WILLIAMS PAPER 2 CANCELLED THE USE OF
SIMULATION TO DEVELOP AN IMPROVED UNDERSTANDING OF HELICOPTER TAIL ROTOR
FAILURES AND DEVELOP AIRCREW EMERGENCY ADVICE BY A.W. MARTYN, P. PHIPPS
AND E. MUSTARD OPTIMAL TRAJECTORIES FOR THE HELICOPTER IN
ONE-ENGINE-INOPERATIVE TERMINAL-AREAOPERATIONS BY R.T.N. CHEN AND Y.
ZHAO NO WRITTEN VERSION IS AVAILABLE FOR PAPER 5 AN INVESTIGATION OF
PRIMARY FLIGHT CONTROL FAILURE IN A PILOTED HELICOPTER BY S.R. GIBBARD
AND L.D. REID SIMULATION DE MISSION POUR LETIGRE (VERSION APPUI
PROTECTION) BY J.F. RIGAL AND G. COLAS MODULAR ROLL-ON / ROLL-OFF DESIGN
CONCEPT OF A ROTORCRAFT SIMULATION CENTER BY K. NIESSEN EVALUATION DE LA
PILOTABILITE DES HELICOPTERES DE TRANSPORT EN UTILISANT LES ESSAIS EN
VOI DE TYPE ADS-33C FORMALISATION DE LA METHODOLOGIE ET DE
L INSTRUMENTATION D ESSAIS BY D. FOURNIER AND D. PAPILLIER PAGE III IV
VIII IX X REFERENCE T KL K2 8 ADS-33 FLIGHT TESTING - LESSONS LEARNED 10
BY C.J. ODDER AND V. GOLLNICK ONERA & DLR COOPERATION ON THE SMART
HELICOPTER CONCEPT 11 - HANDLING QUALITIES DATA BASE FOR HOVER AND LOW
SPEED FLIGHT - BY G. BOUWER, A. TAGHIZAD AND H. MODDEN DEVELOPMENT OF A
TACTICAL HELICOPTER INFRARED SIGNATURE SUPPRESSION (IRSS) SYSTEM 12 BY
P.R. SULLY, D. VANDAM, J. BIRD AND D. LUISI MODEL 412 COMPOSITE TAILBOOM
13 BY G. MUSSETT AND R. FEWS CRASH RESISTANT COMPOSITE SUBFLOOR
STRUCTURES FOR HELICOPTERS 14 BY A.F. JOHNSON, CM. KINDERVATER, H.G.S.J.
THUIS AND J.F.M. WIGGENRAAD PAPER 15 CANCELLED INTRODUCTION OF BERYLLIUM
ALUMINUM CASTINGS IN THE RAH-66 COMANCHE EOSS PROGRAM 16 BY J.P.
SEINBERG, D.P. TETZ AND K.R. RAFTERY REDUCTION OF THE NOISE SIGNATURE OF
THE EUROCOPTER EC 135 17 BY G. NIESL AND G. ARNAUD DUCTED TAIL ROTOR
DESIGNS FOR ROTORCRAFT AND THEIR LOW NOISE FEATURES 18 BY B. EDWARDS, J.
ANDREWS AND C. RAHNKE MESURES EN VOL ET PREVISION DU BRUIT INTERNE D UN
HELICOPTERE ECUREUIL 19 BY A. MORVAN AND J-M. DAVID UPGRADING OF
CLASSICAL LIFTING-LINE THEORY TO OBTAIN ACCURATE FLIGHT MECHANICAL 20
HELICOPTER MODELS: IMPROVED CORRECTION FOR SWEEP EFFECTS BY TH. VAN
HOLTEN ROTORCRAFT - PILOT COUPLING 21 A CRITICAL ISSUE FOR HIGHLY
AUGMENTED HELICOPTERS? BY P.G. HAMEL AN EMPIRICAL CORRECTION METHOD FOR
IMPROVING OFF-AXES RESPONSE PREDICTION 22 IN COMPONENT TYPE FLIGHT
MECHANICS HELICOPTER MODELS BY M.H. MANSUR AND M.B. TISCHLER EFFECT OF
PROPULSION SYSTEM DYNAMICS ON ROTORCRAFT AEROMECHANICAL STABILITY 23 IN
STRAIGHT AND TURNING FLIGHT BY G. GUGLIERI, R. CELI AND F. QUAGLIOTTI
AERODYNAMIC AND ACOUSTICS OF ROTORCRAFT 24 A SURVEY OF THE 75TH FLUID
DYNAMICS PANEL SYMPOSIUM - BERLIN BY H. KORNER AND K. PAHLKE THE
INTEGRATED DEVELOPMENT OF A MEDIUM LIFT MILITARY/CIVIL HELICOPTER 25 BY
J.P. GRAHAM COMPOUND INTEREST - A DIVIDEND FOR THE FUTURE? 26 BY D.V.
HUMPHERSON RAH-66 COMANCHE PROGRAM STATUS 27 BY A.W. LINDEN AND M.H.
STIEGLITZ VI THE APPLICATION OF HELICOPTER MISSION SIMULATION TO SYSTEM
TRADE-OFF ISSUES 28 BY N. TATLOCK, C. SILVESTER AND P. BIRKETT V-22
TECHNICAL CHALLENGES 29 BY S.I. GLUSMAN, R.A. HYLAND AND R.L. MARR
COCKPIT TECHNOLOGIES RESEARCH AT THE FLIGHT RESEARCH LABORATORY OF THE
NATIONAL RESEARCH 30 COUNCIL OF CANADA BY J.M. MORGAN AND S.W. BAILLIE
ADVANCES IN HELICOPTER CAREFREE HANDLING AND CONTROL AUGMENTATION 31 BY
C.P. MASSEY AND J. HOWITT ACTIVE CONTROL OF AEROMECHANICAL STABILITY 32
BY T. KRYSINSKI HELICOPTERS AND NIGHT VISION GOGGLES: A SYNOPSIS OF
CURRENT RESEARCH ON HELICOPTER 33 HANDLING QUALITIES DURING FLIGHT IN
DEGRADED VISUAL ENVIRONMENTS BY S.W. BAILLIE AND J.M. MORGAN THE SOLID
STATE ADAPTIVE ROTOR DESIGN, DEVELOPMENT AND IMPLICATIONS FOR FUTURE 34
ROTORCRAFT BY R. BARRETT AND J. STUTTS VLI
|
adam_txt |
AGARD-CP-592 ADVISORY GROUP FOR AEROSPACE RESEARCH & DEVELOPMENT 7 RUE
ANCELLE, 92200 NEUILLY-SUR-SEINE, FRANCE AGARD CONFERENCE PROCEEDINGS
592 ADVANCES IN ROTORCRAFT TECHNOLOGY (LES AVANCEES EN TECHNOLOGIES POUR
AERONEFS A VOILURE TOURNANTE) PAPERS PRESENTED AT THE FLIGHT VEHICLE
INTEGRATION PANEL SYMPOSIUM HELD IN OTTAWA, CANADA, 27-30MAY 1996. NORTH
ATLANTIC TREATY ORGANIZATION ORGANISATION DU TRAITE DE L'ATLANTIQUE NORD
UB/TIB HANNOVER 115 801 979 89 CONTENTS EXECUTIVE SUMMARY SYNTHESE
THEME/THEME FLIGHT VEHICLE INTEGRATION PANEL ACKNOWLEDGEMENTS TECHNICAL
EVALUATION REPORT BY M. SINCLAIR KEYNOTE ADDRESS 1 BY B.GEN. K.R. PENNIE
KEYNOTE ADDRESS 2 BY GEN. C. BATLLO CERTIFICATION OF MODEL 230
HELICOPTER FOR CATEGORY 'A ELEVATED HELIPAD OPERATIONS BY J. GOLDENBERG,
L. MESLIN, M. BLONDINO AND D. WILLIAMS PAPER 2 CANCELLED THE USE OF
SIMULATION TO DEVELOP AN IMPROVED UNDERSTANDING OF HELICOPTER TAIL ROTOR
FAILURES AND DEVELOP AIRCREW EMERGENCY ADVICE BY A.W. MARTYN, P. PHIPPS
AND E. MUSTARD OPTIMAL TRAJECTORIES FOR THE HELICOPTER IN
ONE-ENGINE-INOPERATIVE TERMINAL-AREAOPERATIONS BY R.T.N. CHEN AND Y.
ZHAO NO WRITTEN VERSION IS AVAILABLE FOR PAPER 5 AN INVESTIGATION OF
PRIMARY FLIGHT CONTROL FAILURE IN A PILOTED HELICOPTER BY S.R. GIBBARD
AND L.D. REID SIMULATION DE MISSION POUR LETIGRE (VERSION APPUI
PROTECTION) BY J.F. RIGAL AND G. COLAS MODULAR ROLL-ON / ROLL-OFF DESIGN
CONCEPT OF A ROTORCRAFT SIMULATION CENTER BY K. NIESSEN EVALUATION DE LA
PILOTABILITE DES HELICOPTERES DE TRANSPORT EN UTILISANT LES ESSAIS EN
VOI DE TYPE ADS-33C FORMALISATION DE LA METHODOLOGIE ET DE
L'INSTRUMENTATION D'ESSAIS BY D. FOURNIER AND D. PAPILLIER PAGE III IV
VIII IX X REFERENCE T KL K2 8 ADS-33 FLIGHT TESTING - LESSONS LEARNED 10
BY C.J. ODDER AND V. GOLLNICK ONERA & DLR COOPERATION ON THE 'SMART
HELICOPTER CONCEPT' 11 - HANDLING QUALITIES DATA BASE FOR HOVER AND LOW
SPEED FLIGHT - BY G. BOUWER, A. TAGHIZAD AND H. MODDEN DEVELOPMENT OF A
TACTICAL HELICOPTER INFRARED SIGNATURE SUPPRESSION (IRSS) SYSTEM 12 BY
P.R. SULLY, D. VANDAM, J. BIRD AND D. LUISI MODEL 412 COMPOSITE TAILBOOM
13 BY G. MUSSETT AND R. FEWS CRASH RESISTANT COMPOSITE SUBFLOOR
STRUCTURES FOR HELICOPTERS 14 BY A.F. JOHNSON, CM. KINDERVATER, H.G.S.J.
THUIS AND J.F.M. WIGGENRAAD PAPER 15 CANCELLED INTRODUCTION OF BERYLLIUM
ALUMINUM CASTINGS IN THE RAH-66 COMANCHE EOSS PROGRAM 16 BY J.P.
SEINBERG, D.P. TETZ AND K.R. RAFTERY REDUCTION OF THE NOISE SIGNATURE OF
THE EUROCOPTER EC 135 17 BY G. NIESL AND G. ARNAUD DUCTED TAIL ROTOR
DESIGNS FOR ROTORCRAFT AND THEIR LOW NOISE FEATURES 18 BY B. EDWARDS, J.
ANDREWS AND C. RAHNKE MESURES EN VOL ET PREVISION DU BRUIT INTERNE D'UN
HELICOPTERE ECUREUIL 19 BY A. MORVAN AND J-M. DAVID UPGRADING OF
CLASSICAL LIFTING-LINE THEORY TO OBTAIN ACCURATE FLIGHT MECHANICAL 20
HELICOPTER MODELS: IMPROVED CORRECTION FOR SWEEP EFFECTS BY TH. VAN
HOLTEN ROTORCRAFT - PILOT COUPLING 21 A CRITICAL ISSUE FOR HIGHLY
AUGMENTED HELICOPTERS? BY P.G. HAMEL AN EMPIRICAL CORRECTION METHOD FOR
IMPROVING OFF-AXES RESPONSE PREDICTION 22 IN COMPONENT TYPE FLIGHT
MECHANICS HELICOPTER MODELS BY M.H. MANSUR AND M.B. TISCHLER EFFECT OF
PROPULSION SYSTEM DYNAMICS ON ROTORCRAFT AEROMECHANICAL STABILITY 23 IN
STRAIGHT AND TURNING FLIGHT BY G. GUGLIERI, R. CELI AND F. QUAGLIOTTI
AERODYNAMIC AND ACOUSTICS OF ROTORCRAFT 24 A SURVEY OF THE 75TH FLUID
DYNAMICS PANEL SYMPOSIUM - BERLIN BY H. KORNER AND K. PAHLKE THE
INTEGRATED DEVELOPMENT OF A MEDIUM LIFT MILITARY/CIVIL HELICOPTER 25 BY
J.P. GRAHAM COMPOUND INTEREST - A DIVIDEND FOR THE FUTURE? 26 BY D.V.
HUMPHERSON RAH-66 COMANCHE PROGRAM STATUS 27 BY A.W. LINDEN AND M.H.
STIEGLITZ VI THE APPLICATION OF HELICOPTER MISSION SIMULATION TO SYSTEM
TRADE-OFF ISSUES 28 BY N. TATLOCK, C. SILVESTER AND P. BIRKETT V-22
TECHNICAL CHALLENGES 29 BY S.I. GLUSMAN, R.A. HYLAND AND R.L. MARR
COCKPIT TECHNOLOGIES RESEARCH AT THE FLIGHT RESEARCH LABORATORY OF THE
NATIONAL RESEARCH 30 COUNCIL OF CANADA BY J.M. MORGAN AND S.W. BAILLIE
ADVANCES IN HELICOPTER CAREFREE HANDLING AND CONTROL AUGMENTATION 31 BY
C.P. MASSEY AND J. HOWITT ACTIVE CONTROL OF AEROMECHANICAL STABILITY 32
BY T. KRYSINSKI HELICOPTERS AND NIGHT VISION GOGGLES: A SYNOPSIS OF
CURRENT RESEARCH ON HELICOPTER 33 HANDLING QUALITIES DURING FLIGHT IN
DEGRADED VISUAL ENVIRONMENTS BY S.W. BAILLIE AND J.M. MORGAN THE SOLID
STATE ADAPTIVE ROTOR DESIGN, DEVELOPMENT AND IMPLICATIONS FOR FUTURE 34
ROTORCRAFT BY R. BARRETT AND J. STUTTS VLI |
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spelling | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 Neuilly-sur-Seine AGARD 1997 Getr. Zählung txt rdacontent n rdamedia nc rdacarrier AGARD conference proceedings 592 Luftfahrttechnik (DE-588)4168244-0 gnd rswk-swf Hubschrauber (DE-588)4025993-6 gnd rswk-swf (DE-588)4143413-4 Aufsatzsammlung gnd-content (DE-588)1071861417 Konferenzschrift gnd-content Hubschrauber (DE-588)4025993-6 s DE-604 Luftfahrttechnik (DE-588)4168244-0 s AGARD conference proceedings 592 (DE-604)BV001900884 GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015344721&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis |
spellingShingle | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 AGARD conference proceedings Luftfahrttechnik (DE-588)4168244-0 gnd Hubschrauber (DE-588)4025993-6 gnd |
subject_GND | (DE-588)4168244-0 (DE-588)4025993-6 (DE-588)4143413-4 (DE-588)1071861417 |
title | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 |
title_auth | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 |
title_exact_search | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 |
title_exact_search_txtP | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 |
title_full | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 |
title_fullStr | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 |
title_full_unstemmed | Advances in rotorcraft technology papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 |
title_short | Advances in rotorcraft technology |
title_sort | advances in rotorcraft technology papers presented at the flight vehicle integration panel symposium held in ottawa canada 27 30 may 1996 |
title_sub | papers presented at the Flight Vehicle Integration Panel Symposium held in Ottawa, Canada, 27-30 May 1996 |
topic | Luftfahrttechnik (DE-588)4168244-0 gnd Hubschrauber (DE-588)4025993-6 gnd |
topic_facet | Luftfahrttechnik Hubschrauber Aufsatzsammlung Konferenzschrift |
url | http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015344721&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA |
volume_link | (DE-604)BV001900884 |