Verfügbarkeit: Aircraft dynamic loads due to flow separation

Aircraft dynamic loads due to flow separation: Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990

Gespeichert in:

Bibliographische Detailangaben
Format:	Buch
Sprache:	English
Veröffentlicht:	Neuilly sur Seine AGARD 1990
Schriftenreihe:	AGARD conference proceedings 483
Schlagworte:	Flugzeug Dynamische Belastung Aerodynamik Konferenzschrift
Online-Zugang:	Inhaltsverzeichnis
Beschreibung:	Getr. Seitenzählung Ill.
ISBN:	9283505824

Internformat

MARC


LEADER	00000nam a2200000zcb4500
001	BV022130019
003	DE-604
005	20221109
007	t
008	921102s1990 a\|\|\| \|\|\|\| 10\|\|\| eng d
020			\|a 9283505824 \|9 92-835-0582-4
035			\|a (OCoLC)635175525
035			\|a (DE-599)BVBBV022130019
040			\|a DE-604 \|b ger
041	0		\|a eng
049			\|a DE-706 \|a DE-83
245	1	0	\|a Aircraft dynamic loads due to flow separation \|b Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
264		1	\|a Neuilly sur Seine \|b AGARD \|c 1990
300			\|a Getr. Seitenzählung \|b Ill.
336			\|b txt \|2 rdacontent
337			\|b n \|2 rdamedia
338			\|b nc \|2 rdacarrier
490	1		\|a AGARD conference proceedings \|v 483
650	0	7	\|a Flugzeug \|0 (DE-588)4017672-1 \|2 gnd \|9 rswk-swf
650	0	7	\|a Dynamische Belastung \|0 (DE-588)4121153-4 \|2 gnd \|9 rswk-swf
650	0	7	\|a Aerodynamik \|0 (DE-588)4000589-6 \|2 gnd \|9 rswk-swf
655		7	\|0 (DE-588)1071861417 \|a Konferenzschrift \|2 gnd-content
689	0	0	\|a Aerodynamik \|0 (DE-588)4000589-6 \|D s
689	0		\|5 DE-604
689	1	0	\|a Flugzeug \|0 (DE-588)4017672-1 \|D s
689	1		\|5 DE-604
689	2	0	\|a Dynamische Belastung \|0 (DE-588)4121153-4 \|D s
689	2		\|5 DE-604
710	2		\|a NATO \|b Structures and Materials Panel \|e Sonstige \|0 (DE-588)5958-4 \|4 oth
830		0	\|a AGARD conference proceedings \|v 483 \|w (DE-604)BV001900884 \|9 483
856	4	2	\|m GBV Datenaustausch \|q application/pdf \|u http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015344640&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA \|3 Inhaltsverzeichnis
999			\|a oai:aleph.bib-bvb.de:BVB01-015344640

Datensatz im Suchindex

_version_	1804136102223675392
adam_text	AGARD-CP-483 NORTH ATLANTICTREATYORGANIZATION ADVISORYGROUPFORAEROSPACERESEARCHANDDEVELOPMENT (ORGANISATIONDUTRAITEDEL ATLANTIQUE NORD) AGARDCONFERENCEPROCEEDINGSNO.483 AIRCRAFTDYNAMICLOADSDUE TO FLOW SEPARATION (LES CONSTRAINTESAERODYNAMIQUES IMPOSEES AUXAERONEFS PAR LE DECOLLEMENTDEL ECOULEMENT) JFO JIJISNNOVER 89 PAPERS PRESENTED ATTHE70THMEETINGOFTHEAGARD STRUCTURESANDMATERIALSPANEL, HELDINSORRENTO,ITALYON 1ST*6THAPRIL 1990. CONTENTS PREFACE/PREFACE STRUCTURES AND MATERIALS PANEL TECHNICAL EVALUATIONREPORT D.G.MABEY SESSIONI -AERODYNAMICBUFFETINPUTCHARACTERISTICS WINDTUNNEL INVESTIGATION AND FLIGHTTESTSOFTAIL BUFFET ONTHECF-18AIRCRAFT 1 BYB.H.K.LEE,D.BROWN,M.ZGELAANDDPOIREL AUNIFIED APPROACH TOBUFFETRESPONSE OFFIGHTER AIRCRAFTEMPENNAGE 2 BYMA.FERMAN, S.R.PATEL,N.H.ZIMMERMANANDG.GESTERNKORN EFFECTSOFTRAILING-EDGEFLAP ONBUFFETCHARACTERISTICS OFASUPERCRITICAL AIRFOIL 3 BYB.H.K.LEE EXPERIMENTAL INVESTIGATIONOFBUFFETONSETANDPENETRATIONON SUPERCRITICAL AIRFOIL AT 4 TRANSONIC SPEEDS BYE.STANEWSKYANDD.BASLER EXPERIMENTALINVESTIGATIONS OFBUFFETEXCITATIONFORCES ON ALOWASPECTRATIO S TRAPEZOIDALHALF-WING ININCOMPRESSIBLEFLOW BYRBUBLITZANDHJZINGEL EXPERIMENTALINVESTIGATION ANDSEMI-EMPIRICALPREDICTIONOFTHEDYNAMICRESPONSEOFA 6 LOW-ASPECT-RATIO TRAPEZOIDALWING DUE TO FLOW SEPARATION BYH.ZINGEL UNSTEADY AERODYNAMIC FORCES ONANOSCILLATINGWING ATHIGHINCIDENCES AND FLOW SEPARATION 7 BYH.W.FORSCHING THE FORWARDMOUNTEDSPOILER ASA SOURCE OFBUFFETEXCITATION 8 BYP.GMYERSANDDL.BIRDSALL INVESTIGATION OFASEMI-EMPIRICAL METHOD TO PREDICT LIMITCYCLE OSCILLATIONS OFMODERN 9 FIGHTERAIRCRAFT BYJJ.MEIJERANDR.J.ZWAAN SESSIONH -IN-FLIGHTANDWINDTUNNELBUFFETINGMEASUREMENTS INTERACTIONBETWEEN THE CANARDANDWING FLOWS ON A MODEL OFATYPICALCOMBATAIRCRAFT 10 BYD.CMABEY,B.L.WELSH ANDGRJPYNE PREDICTIONS OFF-UL TACTAIRCRAFT BUFFETRESPONSE 11 A.M.CUNNINGHAM JRAND CJF.COE THE EFFECT OFWING PLANFORM ONLOW-SPEEDBUFFET 12 BYSJ.ZANANDDJ.MAULL NOUVELLEMETHODE DE DETERMINATION DES FORCES DETREMBLEMENTEN SOUFFLERIE 13 PARRDESTUYNDERETRJBARREAU PAGE III IV REFERENCE T SESSIONIII -AEROELASTICBUFFETINGPREDICTIONTECHNIQUES FORCESAERODYNAMIQUES COUPLEES DUES AU DECROCHAGE INSTATIONNAIRE SURUNEAILE DE 14 GRANDALLONGEMENT OSCILLANTA GRANDE AMPLITUDE PARJJ.COSTES ETD.PETOT UNSTEADY SEPARATEDFLOW PHENOMENA CAUSINGSELF-EXCITED STRUCTURAL OSCILLATIONS 15 BY L.E.ERICSSON UNSTEADYAIRLOADSDUE TO SEPARATED FLOWON AIRFOILS AND WINGS 16 BY J.W.EDWARDS VI
adam_txt	AGARD-CP-483 NORTH ATLANTICTREATYORGANIZATION ADVISORYGROUPFORAEROSPACERESEARCHANDDEVELOPMENT (ORGANISATIONDUTRAITEDEL'ATLANTIQUE NORD) AGARDCONFERENCEPROCEEDINGSNO.483 AIRCRAFTDYNAMICLOADSDUE TO FLOW SEPARATION (LES CONSTRAINTESAERODYNAMIQUES IMPOSEES AUXAERONEFS PAR LE DECOLLEMENTDEL'ECOULEMENT) JFO'JIJISNNOVER 89 PAPERS PRESENTED ATTHE70THMEETINGOFTHEAGARD STRUCTURESANDMATERIALSPANEL, HELDINSORRENTO,ITALYON 1ST*6THAPRIL 1990. CONTENTS PREFACE/PREFACE STRUCTURES AND MATERIALS PANEL TECHNICAL EVALUATIONREPORT D.G.MABEY SESSIONI -AERODYNAMICBUFFETINPUTCHARACTERISTICS WINDTUNNEL INVESTIGATION AND FLIGHTTESTSOFTAIL BUFFET ONTHECF-18AIRCRAFT 1 BYB.H.K.LEE,D.BROWN,M.ZGELAANDDPOIREL AUNIFIED APPROACH TOBUFFETRESPONSE OFFIGHTER AIRCRAFTEMPENNAGE 2 BYMA.FERMAN, S.R.PATEL,N.H.ZIMMERMANANDG.GESTERNKORN EFFECTSOFTRAILING-EDGEFLAP ONBUFFETCHARACTERISTICS OFASUPERCRITICAL AIRFOIL 3 BYB.H.K.LEE EXPERIMENTAL INVESTIGATIONOFBUFFETONSETANDPENETRATIONON SUPERCRITICAL AIRFOIL AT 4 TRANSONIC SPEEDS BYE.STANEWSKYANDD.BASLER EXPERIMENTALINVESTIGATIONS OFBUFFETEXCITATIONFORCES ON ALOWASPECTRATIO S TRAPEZOIDALHALF-WING ININCOMPRESSIBLEFLOW BYRBUBLITZANDHJZINGEL EXPERIMENTALINVESTIGATION ANDSEMI-EMPIRICALPREDICTIONOFTHEDYNAMICRESPONSEOFA 6 LOW-ASPECT-RATIO TRAPEZOIDALWING DUE TO FLOW SEPARATION BYH.ZINGEL UNSTEADY AERODYNAMIC FORCES ONANOSCILLATINGWING ATHIGHINCIDENCES AND FLOW SEPARATION 7 BYH.W.FORSCHING THE FORWARDMOUNTEDSPOILER ASA SOURCE OFBUFFETEXCITATION 8 BYP.GMYERSANDDL.BIRDSALL INVESTIGATION OFASEMI-EMPIRICAL METHOD TO PREDICT LIMITCYCLE OSCILLATIONS OFMODERN 9 FIGHTERAIRCRAFT BYJJ.MEIJERANDR.J.ZWAAN SESSIONH -IN-FLIGHTANDWINDTUNNELBUFFETINGMEASUREMENTS INTERACTIONBETWEEN THE CANARDANDWING FLOWS ON A MODEL OFATYPICALCOMBATAIRCRAFT 10 BYD.CMABEY,B.L.WELSH ANDGRJPYNE PREDICTIONS OFF-UL TACTAIRCRAFT BUFFETRESPONSE 11 A.M.CUNNINGHAM JRAND CJF.COE THE EFFECT OFWING PLANFORM ONLOW-SPEEDBUFFET 12 BYSJ.ZANANDDJ.MAULL NOUVELLEMETHODE DE DETERMINATION DES FORCES DETREMBLEMENTEN SOUFFLERIE 13 PARRDESTUYNDERETRJBARREAU PAGE III IV REFERENCE T SESSIONIII -AEROELASTICBUFFETINGPREDICTIONTECHNIQUES FORCESAERODYNAMIQUES COUPLEES DUES AU DECROCHAGE INSTATIONNAIRE SURUNEAILE DE 14 GRANDALLONGEMENT OSCILLANTA GRANDE AMPLITUDE PARJJ.COSTES ETD.PETOT UNSTEADY SEPARATEDFLOW PHENOMENA CAUSINGSELF-EXCITED STRUCTURAL OSCILLATIONS 15 BY L.E.ERICSSON UNSTEADYAIRLOADSDUE TO SEPARATED FLOWON AIRFOILS AND WINGS 16 BY J.W.EDWARDS VI
any_adam_object	1
any_adam_object_boolean	1
building	Verbundindex
bvnumber	BV022130019
ctrlnum	(OCoLC)635175525 (DE-599)BVBBV022130019
format	Book
fullrecord	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01719nam a2200409zcb4500</leader><controlfield tag="001">BV022130019</controlfield><controlfield tag="003">DE-604</controlfield><controlfield tag="005">20221109 </controlfield><controlfield tag="007">t</controlfield><controlfield tag="008">921102s1990 a\|\|\| \|\|\|\| 10\|\|\| eng d</controlfield><datafield tag="020" ind1=" " ind2=" "><subfield code="a">9283505824</subfield><subfield code="9">92-835-0582-4</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(OCoLC)635175525</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-599)BVBBV022130019</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-604</subfield><subfield code="b">ger</subfield></datafield><datafield tag="041" ind1="0" ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="049" ind1=" " ind2=" "><subfield code="a">DE-706</subfield><subfield code="a">DE-83</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Aircraft dynamic loads due to flow separation</subfield><subfield code="b">Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="a">Neuilly sur Seine</subfield><subfield code="b">AGARD</subfield><subfield code="c">1990</subfield></datafield><datafield tag="300" ind1=" " ind2=" "><subfield code="a">Getr. Seitenzählung</subfield><subfield code="b">Ill.</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="490" ind1="1" ind2=" "><subfield code="a">AGARD conference proceedings</subfield><subfield code="v">483</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Flugzeug</subfield><subfield code="0">(DE-588)4017672-1</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Dynamische Belastung</subfield><subfield code="0">(DE-588)4121153-4</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="650" ind1="0" ind2="7"><subfield code="a">Aerodynamik</subfield><subfield code="0">(DE-588)4000589-6</subfield><subfield code="2">gnd</subfield><subfield code="9">rswk-swf</subfield></datafield><datafield tag="655" ind1=" " ind2="7"><subfield code="0">(DE-588)1071861417</subfield><subfield code="a">Konferenzschrift</subfield><subfield code="2">gnd-content</subfield></datafield><datafield tag="689" ind1="0" ind2="0"><subfield code="a">Aerodynamik</subfield><subfield code="0">(DE-588)4000589-6</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="0" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="1" ind2="0"><subfield code="a">Flugzeug</subfield><subfield code="0">(DE-588)4017672-1</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="1" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="689" ind1="2" ind2="0"><subfield code="a">Dynamische Belastung</subfield><subfield code="0">(DE-588)4121153-4</subfield><subfield code="D">s</subfield></datafield><datafield tag="689" ind1="2" ind2=" "><subfield code="5">DE-604</subfield></datafield><datafield tag="710" ind1="2" ind2=" "><subfield code="a">NATO</subfield><subfield code="b">Structures and Materials Panel</subfield><subfield code="e">Sonstige</subfield><subfield code="0">(DE-588)5958-4</subfield><subfield code="4">oth</subfield></datafield><datafield tag="830" ind1=" " ind2="0"><subfield code="a">AGARD conference proceedings</subfield><subfield code="v">483</subfield><subfield code="w">(DE-604)BV001900884</subfield><subfield code="9">483</subfield></datafield><datafield tag="856" ind1="4" ind2="2"><subfield code="m">GBV Datenaustausch</subfield><subfield code="q">application/pdf</subfield><subfield code="u">http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015344640&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA</subfield><subfield code="3">Inhaltsverzeichnis</subfield></datafield><datafield tag="999" ind1=" " ind2=" "><subfield code="a">oai:aleph.bib-bvb.de:BVB01-015344640</subfield></datafield></record></collection>
genre	(DE-588)1071861417 Konferenzschrift gnd-content
genre_facet	Konferenzschrift
id	DE-604.BV022130019
illustrated	Illustrated
index_date	2024-07-02T16:16:47Z
indexdate	2024-07-09T20:51:03Z
institution	BVB
institution_GND	(DE-588)5958-4
isbn	9283505824
language	English
oai_aleph_id	oai:aleph.bib-bvb.de:BVB01-015344640
oclc_num	635175525
open_access_boolean
owner	DE-706 DE-83
owner_facet	DE-706 DE-83
physical	Getr. Seitenzählung Ill.
publishDate	1990
publishDateSearch	1990
publishDateSort	1990
publisher	AGARD
record_format	marc
series	AGARD conference proceedings
series2	AGARD conference proceedings
spelling	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990 Neuilly sur Seine AGARD 1990 Getr. Seitenzählung Ill. txt rdacontent n rdamedia nc rdacarrier AGARD conference proceedings 483 Flugzeug (DE-588)4017672-1 gnd rswk-swf Dynamische Belastung (DE-588)4121153-4 gnd rswk-swf Aerodynamik (DE-588)4000589-6 gnd rswk-swf (DE-588)1071861417 Konferenzschrift gnd-content Aerodynamik (DE-588)4000589-6 s DE-604 Flugzeug (DE-588)4017672-1 s Dynamische Belastung (DE-588)4121153-4 s NATO Structures and Materials Panel Sonstige (DE-588)5958-4 oth AGARD conference proceedings 483 (DE-604)BV001900884 483 GBV Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015344640&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis
spellingShingle	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990 AGARD conference proceedings Flugzeug (DE-588)4017672-1 gnd Dynamische Belastung (DE-588)4121153-4 gnd Aerodynamik (DE-588)4000589-6 gnd
subject_GND	(DE-588)4017672-1 (DE-588)4121153-4 (DE-588)4000589-6 (DE-588)1071861417
title	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
title_auth	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
title_exact_search	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
title_exact_search_txtP	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
title_full	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
title_fullStr	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
title_full_unstemmed	Aircraft dynamic loads due to flow separation Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
title_short	Aircraft dynamic loads due to flow separation
title_sort	aircraft dynamic loads due to flow separation papers presented at the 70 meeting of the agard structures and materials panel held in sorrento italy on 1 6 april 1990
title_sub	Papers presented at the 70. Meeting of the AGARD Structures and Materials Panel, held in Sorrento, Italy on 1. - 6. April 1990
topic	Flugzeug (DE-588)4017672-1 gnd Dynamische Belastung (DE-588)4121153-4 gnd Aerodynamik (DE-588)4000589-6 gnd
topic_facet	Flugzeug Dynamische Belastung Aerodynamik Konferenzschrift
url	http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=015344640&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
volume_link	(DE-604)BV001900884
work_keys_str_mv	AT natostructuresandmaterialspanel aircraftdynamicloadsduetoflowseparationpaperspresentedatthe70meetingoftheagardstructuresandmaterialspanelheldinsorrentoitalyon16april1990

Verfügbarkeit

Es ist kein Print-Exemplar vorhanden.

Fernleihe Bestellen Achtung: Nicht im THWS-Bestand! Inhaltsverzeichnis

MARC

Datensatz im Suchindex

Es ist kein Print-Exemplar vorhanden.

Ähnliche Einträge