Verfügbarkeit: Vortex wakes of aircrafts

Vortex wakes of aircrafts:

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Bibliographische Detailangaben
Hauptverfasser:	Ginevskij, Aron S. (VerfasserIn), Zhelannikov, A. I. (VerfasserIn)
Format:	Buch
Sprache:	English
Veröffentlicht:	Berlin [u.a.] Springer 2009
Schriftenreihe:	Foundations of engineering mechanics
Schlagworte:	Start Flugzeug Mathematisches Modell Wirbelschleppe Landung
Online-Zugang:	Inhaltsverzeichnis Inhaltsverzeichnis
Beschreibung:	XV, 154 S. Ill., graph. Darst.
ISBN:	9783642017599

Internformat

MARC


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Datensatz im Suchindex

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adam_text	CONTENTS ABSTRACT VIII FOREWORD IX INTRODUCTION XI CHAPTER 1. GENERAL 1 1 . 1 . ATMOSPHERIC TURBULENCE 1 1.2. AIRCRAFT VORTEX WAKE 4 1.3. TURBULENCE CHARACTERISTICS OF THE VORTEX WAKE 9 1.4. PRESENT-DAY METHODS FOR NUMERICAL SIMULATION OF VORTEX WAKES BEHIND TRUNK-ROUTE AIRCRAFT 10 CHAPTER 2. DISCRETE VORTEX METHOD 13 2.1 . PROBLEM STATEMENT 13 2.2. FUNDAMENTALS OF THE DISCRETE VORTEX METHOD 17 2.3 . POINT VORTEX 18 2.4. VORTEX SEGMENT 19 2.5 . CLOSED VORTEX FRAME 20 2.6. NUMERICAL MODELING OF FREE TURBULENCE IN SEPARATED AND JET FLOWS IN THE FRAMEWORK OF THE DISCRETE VORTEX METHOD 21 CHAPTER 3 . THE NEAR VORTEX WAKE BEHIND A SINGLE AIRCRAFT 33 3.1 . AIRCRAFT GEOMETRY REPRESENTATION 33 3.2. VORTICITY PANEL REPRESENTATION 34 3.3 . PECULIARITIES OF FLOW SIMULATION AROUND TRUNK-ROUTE AIRCRAFT 34 3.4. THE CHARACTERISTICS OF THE NEAR VORTEX WAKE BEHIND SOME AIRCRAFT .. . 35 CHAPTER 4. FAR VORTEX WAKE BEHIND A TURBOJET AIRCRAFT 39 4.1. THE ALGORITHM FOR COMPUTATION OF THE FAR VORTEX WAKE BEHIND AIRCRAFT 39 BIBLIOGRAFISCHE INFORMATIONEN HTTP://D-NB.INFO/995654646 DIGITALISIERT DURCH VI CONTENTS 4.2. MATHEMATICAL MODEL OF THE FAR VORTEX WAKE 41 4.3 . CHECK FOR THE EXISTENCE AND UNIQUENESS OF THE SOLUTION 42 4.4. SIMILARITY CONSIDERATIONS FOR FLOW IN THE FAR VORTEX WAKE 47 4.5 . A UNIVERSAL PROCEDURE FOR TRANSITION TO THE MATHEMATICAL MODEL OF THE FAR VORTEX WAKE 50 4.6. CONSIDERATION OF THE STATE OF THE ATMOSPHERE 53 4.7. VERIFICATION OF THE METHOD AND PREDICTED RESULT S 55 4.8 . THE CHARACTERISTICS OF THE VORTEX WAKE BEHIND THE 11-76 AIRCRAFT 57 4.9 . THE CHARACTERISTICS OF THE VORTEX WAKE BEHIND THE AN-124, B-747 AND A-380 AIRCRAFT 61 CHAPTER 5. VORTEX WAKE S BEHIND PROPELLER-DRIVEN AIRCRAFT 71 5.1 . PROBLEM STATEMENT 71 5.2. THE EFFECT OF PROPELLERS ON THE FAR VORTEX WAKE CHARACTERISTICS 72 5.3. ON A RATIONAL NUMBER OF VORTICES FOR MODELING A PROPELLER 76 5.4. EXAMPLES OF COMPUTED FAR VORTEX WAKE CHARACTERISTICS OF PROPELLER DRIVEN AIRCRAFT IN COMPARISON WITH EXPERIMENTAL DATA 78 5.5. THE CHARACTERISTICS OF THE VORTEX WAKE BEHIND THE AN-26 AIRCRAFT. .. . 79 5.6. THE CHARACTERISTICS OF THE VORTEX WAKE BEHIND THE AN-12 AIRCRAFT 84 5.7. THE CHARACTERISTICS OF THE VORTEX WAKE BEHIND THE C-130 AIRCRAFT. .. . 90 CHAPTER 6. WIND FLOW OVER ROUGH TERRAIN 99 6. 1 . BASIC CONDITIONS 99 6.2. PROBLEM STATEMENT 99 6.3 . A SOLUTION TECHNIQUE. TERRAIN REPRESENTATION 100 6.4. EXAMPLES OF AIR FLOW COMPUTATIONS 100 CHAPTER 7. SIMULATION OF THE FAR VORTEX WAKE OF AN AIRCRAFT AT TAKEOFF AND LANDING 105 7.1. PROBLEM STATEMENT 105 7.2. SIMULATION OF AN AIRCRAFT S NEAR VORTEX WAKE. LINEAR THEORY 108 7.3. AN APPROXIMATE COMPUTATION OF AN AIRCRAFT S FAR VORTEX WAKE 115 7.4. GENERATION OF CROSSFLOW BY VORTEX TUBES . TURBULENT BOUNDARY LAYER COMPUTATION 116 7.5. COMPUTATION OF THE FAR VORTEX WAKE BEHIND THE B-727 AIRCRAFT WITH ACCOUNT FOR THE EFFECT OF THE BOUNDARY LAYER ON AN AERODROME S SURFACE. COMPARISON BETWEEN COMPUTATIONAL RESULTS AND FLIGHT TEST DATA 118 7.6. COMPUTATION OF THE FAR VORTEX WAKE OF RUSSIAN-BUILT TU-204 AND 11-96 TRUNK-ROUTE AIRCRAFT AT LANDING 122 7.7. ON THE VISUALIZATION OF AN AIRCRAFT S FAR VORTEX WAKE NEAR THE GROUND 125 7.8. CONCLUSIONS AND PROSPECTS 126 CONTENTS VII CHAPTER 8. AERODYNAMIC LOADS ON AIRCRAFT ENCOUNTERING VORTEX WAKE S OF OTHER AIRCRAFT 129 8.1 . PROBLEM STATEMENT 129 8.2. A SOLUTION TECHNIQUE 130 8.3. VERIFICATION OF THE METHOD AND PREDICTED RESULTS 131 8.4. THE AERODYNAMIC LOADS ON AIRCRAFT IN THE FAR VORTEX WAKES OF PRECEDING AIRCRAFT 134 8.5. PREDICTION OF THE EFFECT OF WIND FLOW OVER ROUGH TERRAIN ON THE AERODYNAMIC LOADS EXPERIENCED BY AN AIRCRAFT 137 8.6. NUMERICAL PREDICTION OF AN AIRCRAFT S DYNAMICS IN A VORTEX WAKE ... . 144 REFERENCES 149
any_adam_object	1
author	Ginevskij, Aron S. Zhelannikov, A. I.
author_facet	Ginevskij, Aron S. Zhelannikov, A. I.
author_role	aut aut
author_sort	Ginevskij, Aron S.
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building	Verbundindex
bvnumber	BV035796030
classification_rvk	ZO 7250
ctrlnum	(OCoLC)437036615 (DE-599)DNB995654646
dewey-full	629.13232015118
dewey-hundreds	600 - Technology (Applied sciences)
dewey-ones	629 - Other branches of engineering
dewey-raw	629.13232015118
dewey-search	629.13232015118
dewey-sort	3629.13232015118
dewey-tens	620 - Engineering and allied operations
discipline	Maschinenbau / Maschinenwesen Verkehr / Transport
format	Book
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spelling	Ginevskij, Aron S. Verfasser aut Vortex wakes of aircrafts A. S. Ginevsky ; A. I. Zhelannikov Berlin [u.a.] Springer 2009 XV, 154 S. Ill., graph. Darst. txt rdacontent n rdamedia nc rdacarrier Foundations of engineering mechanics Start (DE-588)4182937-2 gnd rswk-swf Flugzeug (DE-588)4017672-1 gnd rswk-swf Mathematisches Modell (DE-588)4114528-8 gnd rswk-swf Wirbelschleppe (DE-588)4384015-2 gnd rswk-swf Landung (DE-588)4120649-6 gnd rswk-swf Flugzeug (DE-588)4017672-1 s Start (DE-588)4182937-2 s Landung (DE-588)4120649-6 s Wirbelschleppe (DE-588)4384015-2 s Mathematisches Modell (DE-588)4114528-8 s DE-604 Zhelannikov, A. I. Verfasser aut Erscheint auch als Online-Ausgabe 978-3-642-01760-5 http://d-nb.info/995654646/04 Inhaltsverzeichnis DNB Datenaustausch application/pdf http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018655322&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA Inhaltsverzeichnis
spellingShingle	Ginevskij, Aron S. Zhelannikov, A. I. Vortex wakes of aircrafts Start (DE-588)4182937-2 gnd Flugzeug (DE-588)4017672-1 gnd Mathematisches Modell (DE-588)4114528-8 gnd Wirbelschleppe (DE-588)4384015-2 gnd Landung (DE-588)4120649-6 gnd
subject_GND	(DE-588)4182937-2 (DE-588)4017672-1 (DE-588)4114528-8 (DE-588)4384015-2 (DE-588)4120649-6
title	Vortex wakes of aircrafts
title_auth	Vortex wakes of aircrafts
title_exact_search	Vortex wakes of aircrafts
title_full	Vortex wakes of aircrafts A. S. Ginevsky ; A. I. Zhelannikov
title_fullStr	Vortex wakes of aircrafts A. S. Ginevsky ; A. I. Zhelannikov
title_full_unstemmed	Vortex wakes of aircrafts A. S. Ginevsky ; A. I. Zhelannikov
title_short	Vortex wakes of aircrafts
title_sort	vortex wakes of aircrafts
topic	Start (DE-588)4182937-2 gnd Flugzeug (DE-588)4017672-1 gnd Mathematisches Modell (DE-588)4114528-8 gnd Wirbelschleppe (DE-588)4384015-2 gnd Landung (DE-588)4120649-6 gnd
topic_facet	Start Flugzeug Mathematisches Modell Wirbelschleppe Landung
url	http://d-nb.info/995654646/04 http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&local_base=BVB01&doc_number=018655322&sequence=000001&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA
work_keys_str_mv	AT ginevskijarons vortexwakesofaircrafts AT zhelannikovai vortexwakesofaircrafts

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