東華大學圖書館 |

Language: English

Help

回圖書館首頁

手機版館藏查詢

Back

Switch To: Labeled | MARC Mode | ISBD

Hypersonic curved compression inlet ...

Zhang, Kunyuan.

Linked to FindBook

Google Book

Amazon

博客來

Hypersonic curved compression inlet and its inverse design

Record Type:	Electronic resources : Monograph/item
Title/Author:	Hypersonic curved compression inlet and its inverse design/ by Kunyuan Zhang.
Author:	Zhang, Kunyuan.
Published:	Singapore :Springer Singapore : : 2020.,
Description:	xiv, 332 p. :ill., digital ;24 cm.
[NT 15003449]:	Introduction -- Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field -- Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface -- Inverse Design of Compression Inlet with Specified Exit Aerodynamic Parameters -- Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design of Axisymmetric Reference Flow Field on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet -- Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet -- Features and Drag Reduction Analysis of Drag in Hypersonic Inlet -- The Development of Curved Compression and Application Prospect.
Contained By:	Springer eBooks
Subject:	Aerodynamics, Hypersonic. -
Online resource:	https://doi.org/10.1007/978-981-15-0727-4
ISBN:	9789811507274

Hypersonic curved compression inlet and its inverse design
Zhang, Kunyuan.

Hypersonic curved compression inlet and its inverse design[electronic resource] /by Kunyuan Zhang. - Singapore :Springer Singapore :2020. - xiv, 332 p. :ill., digital ;24 cm. - Advanced topics in science and technology in China,v.561995-6819 ;. - Advanced topics in science and technology in China ;v.56..

Introduction -- Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field -- Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface -- Inverse Design of Compression Inlet with Specified Exit Aerodynamic Parameters -- Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design of Axisymmetric Reference Flow Field on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet -- Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet -- Features and Drag Reduction Analysis of Drag in Hypersonic Inlet -- The Development of Curved Compression and Application Prospect.

This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic-hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the author's research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s. This book introduces the research history, working characteristics, performance calculation and aerodynamic configuration design method of this compression mode in detail. It also describes method of estimating the minimum drag in inlet and drag reduction effect of curved compression and proposes a new index for evaluating unit area compression efficiency of the inlet. Further, it reviews the relevant recent research on curved compression. As such it is a valuable resource for students, researchers and scientists in the fields of hypersonic propulsion and aeronautics.

ISBN: 9789811507274

Standard No.: 10.1007/978-981-15-0727-4doiSubjects--Topical Terms:

661552
Aerodynamics, Hypersonic.

LC Class. No.: TL571.5 / .Z436 2020

Dewey Class. No.: 629.132306

Hypersonic curved compression inlet and its inverse design
LDR:02841nmm a2200349 a 4500 001 2215859
003 DE-He213
005 20200703150633.0
006 m d
007 cr nn 008maaau
008 201120s2020 si s 0 eng d
020 $a 9789811507274 $q (electronic bk.)
020 $a 9789811507267 $q (paper)
024 7 $a 10.1007/978-981-15-0727-4 $2 doi
035 $a 978-981-15-0727-4
040 $a GP $c GP
041 0 $a eng
050 4 $a TL571.5 $b .Z436 2020
072 7 $a PHDF $2 bicssc
072 7 $a SCI085000 $2 bisacsh
072 7 $a PHDF $2 thema
072 7 $a PHDF $2 thema
082 0 4 $a 629.132306 $2 23
090 $a TL571.5 $b .Z63 2020
100 1 $a Zhang, Kunyuan. $3 3447736
245 1 0 $a Hypersonic curved compression inlet and its inverse design $h [electronic resource] / $c by Kunyuan Zhang.
260 $a Singapore : $b Springer Singapore : $b Imprint: Springer, $c 2020.
300 $a xiv, 332 p. : $b ill., digital ; $c 24 cm.
490 1 $a Advanced topics in science and technology in China, $x 1995-6819 ; $v v.56
505 0 $a Introduction -- Calculation and Analysis Method of Two Dimensional Curved Shock Wave Curved Compression Flow Field -- Forward Design of Two Dimensional Curved Shock Wave Curved Compression Surface -- Inverse Design of Compression Inlet with Specified Exit Aerodynamic Parameters -- Inverse Design of Curved Shock Wave Compression Surface on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design of Axisymmetric Reference Flow Field on Basis of Specified Wall Aerodynamic Parameters -- Inverse Design and Experiment of Hypersonic Curved Shock Wave Compression Inlet -- Concept of Hypersonic Adaptive Variable Geometric Curved Compression Inlet -- Features and Drag Reduction Analysis of Drag in Hypersonic Inlet -- The Development of Curved Compression and Application Prospect.
520 $a This book presents systematic research results on curved shock wave-curved compression surface applied to the compression surface design of supersonic-hypersonic inlet, which is a brand new inlet design. The concept of supersonic inlet curved compression discussed originated from the author's research at the Deutsches Zentrum fur Luft- und Raumfahrt (DLR SM-ES) in the early 1990s. This book introduces the research history, working characteristics, performance calculation and aerodynamic configuration design method of this compression mode in detail. It also describes method of estimating the minimum drag in inlet and drag reduction effect of curved compression and proposes a new index for evaluating unit area compression efficiency of the inlet. Further, it reviews the relevant recent research on curved compression. As such it is a valuable resource for students, researchers and scientists in the fields of hypersonic propulsion and aeronautics.
650 0 $a Aerodynamics, Hypersonic. $3 661552
650 0 $a Curves. $3 552607
650 1 4 $a Fluid- and Aerodynamics. $3 1066670
650 2 4 $a Engineering Fluid Dynamics. $3 891349
650 2 4 $a Aerospace Technology and Astronautics. $3 928116
710 2 $a SpringerLink (Online service) $3 836513
773 0 $t Springer eBooks
830 0 $a Advanced topics in science and technology in China ; $v v.56. $3 3447737
856 4 0 $u https://doi.org/10.1007/978-981-15-0727-4
950 $a Physics and Astronomy (Springer-11651)