Hypersonics [electronic resource] : Volume 1 Defining the Hypersonic Environment / by BERTIN, GLOWINSKI, PERIAUX.
Erişim Adresi
ISBN
9781468491876
Dil Kodu
İngilizce
Yer Numarası
DK/16292
Yazar
Basım Bildirimi
1st ed. 1989.
Yayın Bilgisi
Boston, MA : Birkhäuser Boston : Imprint: Birkhäuser, 1989.
Fiziksel Niteleme
X, 549 p. 200 illus. online resource.
Dizi
Progress in Scientific Computing ; 8
İçindekiler Notu
General Characterization of Hypersonic Flows -- to the Hypersonic Phenomena of Hermes -- Industrial Methodologies for the Design of Hypersonic Vehicles -- Defining the Aerothermodynamic Methodology -- Hypersonic Airbreathing Vehicle Design (Focus on Aero-Space Plane) -- Physico-Chemical Gas Dynamics and Its Relation to Hypersonic Flow -- Real Gas Effects -- Effects of Thermochemistry, Nonequilibrium, and Surface Catalysis on the Design of Hypersonic Vehicles -- Non-Equilibrium Effects in High Speed Flows: Modeling and Experimentation -- Air Dissociation Thermochemistry and Problems Resulting from the Coupling of Flow and Chemistry -- Rarefied Gas Dynamics for Spacecraft -- Rarefied Gas Dynamics -- Permissions.
Özet, vb.
Tbe task of defining the aerothermodynamic environment for a vehicle flying through the air at hypersonic speeds offers diverse challenges to the designer. He must integrate a wide variety of scientific and technical disciplines, blending mathematical modeling, computational methods, and experimental measurements. Many of the manned reentry vehicles are relatively blunt or fly at very high angles of attack (so that the drag is relatively large) and enter the atmosphere at a relatively low entry angle. As a result, the hypersonic deceleration occurs at very high altitudes. Because the conversion of kinetic energy to internal energy modes occurs in a low density environment, the flow-field chemistry is an im portant consideration. Experiments on the U. S. Space Shuttle demonstrated the importance of nonequilibrium flow and surface catalycity on the heating to the vehicle. To determine the aerothermodynamic environment of other vehicles op erating hypersonically at very high altitudes, e. g. , the Aero-Assisted Space Transfer Vehicle, the designer may have to consider viscous/inviscid interactions and the modeling of noncontinuum flows. Configurations that have a relatively high ballistic coefficient (such as slender reentry vehicles) and reenter the atmosphere at relatively high angles of attack experience severe heating rates and high dynamic pressures, but only for a short period of time. For these vehicles, continuum flow models incorporating equi librium chemistry are reasonable.
Konu
Social sciences.
Humanities.
Humanities and Social Sciences.
Humanities.
Humanities and Social Sciences.
Diğer Yazarlar
Kurum Adı
Eseri Alıntıla
Referansları kullanmadan önce gözden geçirmeniz ve varsa gerekli düzeltmeleri yapmanız önerilir.
Dijital Kaynak
MARC Görünümü
LEADER 04830nam a22005655i 4500
001 815056
003 TR_AnAIT
005 20260130212337
007 cr nn 008mamaa
008 121204s1989 xxu| s |||| 0|eng d
020 |a9781468491876|9978-1-4684-9187-6
024 7 |a10.1007/978-1-4684-9187-6|2doi
041 |aeng
049 |aTürk Tarih Kurumu Kütüphanesi
050 4|aH1-99
050 4|aAZ19.2-999
072 7|aGT|2bicssc
072 7|aNON000000|2bisacsh
072 7|aGT|2thema
082 04|a300|223
082 04|a001.3|223
090 |aDK/16292
100 1 |aBERTIN.|eauthor.|4aut|4http://id.loc.gov/vocabulary/relators/aut
245 10|aHypersonics|h[electronic resource] :|bVolume 1 Defining the Hypersonic Environment /|cby BERTIN, GLOWINSKI, PERIAUX.
250 |a1st ed. 1989.
264 1|aBoston, MA :|bBirkhäuser Boston :|bImprint: Birkhäuser,|c1989.
300 |aX, 549 p. 200 illus.|bonline resource.
336 |atext|btxt|2rdacontent
337 |acomputer|bc|2rdamedia
338 |aonline resource|bcr|2rdacarrier
347 |atext file|bPDF|2rda
490 1 |aProgress in Scientific Computing ;|v8
505 0 |aGeneral Characterization of Hypersonic Flows -- to the Hypersonic Phenomena of Hermes -- Industrial Methodologies for the Design of Hypersonic Vehicles -- Defining the Aerothermodynamic Methodology -- Hypersonic Airbreathing Vehicle Design (Focus on Aero-Space Plane) -- Physico-Chemical Gas Dynamics and Its Relation to Hypersonic Flow -- Real Gas Effects -- Effects of Thermochemistry, Nonequilibrium, and Surface Catalysis on the Design of Hypersonic Vehicles -- Non-Equilibrium Effects in High Speed Flows: Modeling and Experimentation -- Air Dissociation Thermochemistry and Problems Resulting from the Coupling of Flow and Chemistry -- Rarefied Gas Dynamics for Spacecraft -- Rarefied Gas Dynamics -- Permissions.
520 |aTbe task of defining the aerothermodynamic environment for a vehicle flying through the air at hypersonic speeds offers diverse challenges to the designer. He must integrate a wide variety of scientific and technical disciplines, blending mathematical modeling, computational methods, and experimental measurements. Many of the manned reentry vehicles are relatively blunt or fly at very high angles of attack (so that the drag is relatively large) and enter the atmosphere at a relatively low entry angle. As a result, the hypersonic deceleration occurs at very high altitudes. Because the conversion of kinetic energy to internal energy modes occurs in a low density environment, the flow-field chemistry is an im portant consideration. Experiments on the U. S. Space Shuttle demonstrated the importance of nonequilibrium flow and surface catalycity on the heating to the vehicle. To determine the aerothermodynamic environment of other vehicles op erating hypersonically at very high altitudes, e. g. , the Aero-Assisted Space Transfer Vehicle, the designer may have to consider viscous/inviscid interactions and the modeling of noncontinuum flows. Configurations that have a relatively high ballistic coefficient (such as slender reentry vehicles) and reenter the atmosphere at relatively high angles of attack experience severe heating rates and high dynamic pressures, but only for a short period of time. For these vehicles, continuum flow models incorporating equi librium chemistry are reasonable.
532 8 |aAccessibility summary: This PDF is not accessible. It is based on scanned pages and does not support features such as screen reader compatibility or described non-text content (images, graphs etc). However, it likely supports searchable and selectable text based on OCR (Optical Character Recognition). Users with accessibility needs may not be able to use this content effectively. Please contact us at accessibilitysupport@springernature.com if you require assistance or an alternative format.
532 8 |aInaccessible, or known limited accessibility
532 8 |aNo reading system accessibility options actively disabled
532 8 |aPublisher contact for further accessibility information: accessibilitysupport@springernature.com
650 0|aSocial sciences.
650 0|aHumanities.
650 14|aHumanities and Social Sciences.
700 1 |aGLOWINSKI.|eauthor.|4aut|4http://id.loc.gov/vocabulary/relators/aut
700 1 |aPERIAUX.|eauthor.|4aut|4http://id.loc.gov/vocabulary/relators/aut
710 2 |aSpringerLink (Online service)
773 0 |tSpringer Nature eBook
776 08|iPrinted edition:|z9780817634209
776 08|iPrinted edition:|z9781468491883
776 08|iPrinted edition:|z9781468491890
830 0|aProgress in Scientific Computing ;|v8
856 40|uhttps://doi.org/10.1007/978-1-4684-9187-6
912 |aZDB-2-SHU
912 |aZDB-2-BAE
950 |aHumanities, Social Sciences and Law (SpringerNature-11648)
001 815056
003 TR_AnAIT
005 20260130212337
007 cr nn 008mamaa
008 121204s1989 xxu| s |||| 0|eng d
020 |a9781468491876|9978-1-4684-9187-6
024 7 |a10.1007/978-1-4684-9187-6|2doi
041 |aeng
049 |aTürk Tarih Kurumu Kütüphanesi
050 4|aH1-99
050 4|aAZ19.2-999
072 7|aGT|2bicssc
072 7|aNON000000|2bisacsh
072 7|aGT|2thema
082 04|a300|223
082 04|a001.3|223
090 |aDK/16292
100 1 |aBERTIN.|eauthor.|4aut|4http://id.loc.gov/vocabulary/relators/aut
245 10|aHypersonics|h[electronic resource] :|bVolume 1 Defining the Hypersonic Environment /|cby BERTIN, GLOWINSKI, PERIAUX.
250 |a1st ed. 1989.
264 1|aBoston, MA :|bBirkhäuser Boston :|bImprint: Birkhäuser,|c1989.
300 |aX, 549 p. 200 illus.|bonline resource.
336 |atext|btxt|2rdacontent
337 |acomputer|bc|2rdamedia
338 |aonline resource|bcr|2rdacarrier
347 |atext file|bPDF|2rda
490 1 |aProgress in Scientific Computing ;|v8
505 0 |aGeneral Characterization of Hypersonic Flows -- to the Hypersonic Phenomena of Hermes -- Industrial Methodologies for the Design of Hypersonic Vehicles -- Defining the Aerothermodynamic Methodology -- Hypersonic Airbreathing Vehicle Design (Focus on Aero-Space Plane) -- Physico-Chemical Gas Dynamics and Its Relation to Hypersonic Flow -- Real Gas Effects -- Effects of Thermochemistry, Nonequilibrium, and Surface Catalysis on the Design of Hypersonic Vehicles -- Non-Equilibrium Effects in High Speed Flows: Modeling and Experimentation -- Air Dissociation Thermochemistry and Problems Resulting from the Coupling of Flow and Chemistry -- Rarefied Gas Dynamics for Spacecraft -- Rarefied Gas Dynamics -- Permissions.
520 |aTbe task of defining the aerothermodynamic environment for a vehicle flying through the air at hypersonic speeds offers diverse challenges to the designer. He must integrate a wide variety of scientific and technical disciplines, blending mathematical modeling, computational methods, and experimental measurements. Many of the manned reentry vehicles are relatively blunt or fly at very high angles of attack (so that the drag is relatively large) and enter the atmosphere at a relatively low entry angle. As a result, the hypersonic deceleration occurs at very high altitudes. Because the conversion of kinetic energy to internal energy modes occurs in a low density environment, the flow-field chemistry is an im portant consideration. Experiments on the U. S. Space Shuttle demonstrated the importance of nonequilibrium flow and surface catalycity on the heating to the vehicle. To determine the aerothermodynamic environment of other vehicles op erating hypersonically at very high altitudes, e. g. , the Aero-Assisted Space Transfer Vehicle, the designer may have to consider viscous/inviscid interactions and the modeling of noncontinuum flows. Configurations that have a relatively high ballistic coefficient (such as slender reentry vehicles) and reenter the atmosphere at relatively high angles of attack experience severe heating rates and high dynamic pressures, but only for a short period of time. For these vehicles, continuum flow models incorporating equi librium chemistry are reasonable.
532 8 |aAccessibility summary: This PDF is not accessible. It is based on scanned pages and does not support features such as screen reader compatibility or described non-text content (images, graphs etc). However, it likely supports searchable and selectable text based on OCR (Optical Character Recognition). Users with accessibility needs may not be able to use this content effectively. Please contact us at accessibilitysupport@springernature.com if you require assistance or an alternative format.
532 8 |aInaccessible, or known limited accessibility
532 8 |aNo reading system accessibility options actively disabled
532 8 |aPublisher contact for further accessibility information: accessibilitysupport@springernature.com
650 0|aSocial sciences.
650 0|aHumanities.
650 14|aHumanities and Social Sciences.
700 1 |aGLOWINSKI.|eauthor.|4aut|4http://id.loc.gov/vocabulary/relators/aut
700 1 |aPERIAUX.|eauthor.|4aut|4http://id.loc.gov/vocabulary/relators/aut
710 2 |aSpringerLink (Online service)
773 0 |tSpringer Nature eBook
776 08|iPrinted edition:|z9780817634209
776 08|iPrinted edition:|z9781468491883
776 08|iPrinted edition:|z9781468491890
830 0|aProgress in Scientific Computing ;|v8
856 40|uhttps://doi.org/10.1007/978-1-4684-9187-6
912 |aZDB-2-SHU
912 |aZDB-2-BAE
950 |aHumanities, Social Sciences and Law (SpringerNature-11648)
Materyaller
Depodan talep edilen materyal sadece kütüphane içerisinde kullanılmaktadır.
Materyal dışarıya ödünç verilmemektedir.
Materyal dışarıya ödünç verilmemektedir.
