Hypersonic curved compression inlet and its inverse design. (2020)

• Record Type: Book
• Further Information: Note: Kunyuan Zhang.
• Other Names: Zhang, Kunyuan
• Contents: 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.
• Publisher Details: Singapore : Springer
• Publication Date: 2020
• Extent: 1 online resource
• Subjects: 629.132/306; Aerodynamics, Hypersonic; Curves; Aerodynamics, Hypersonic; Curves; Electronic books; Electronic books
• Languages: English
• ISBNs: 9789811507274; 9811507279
• Related ISBNs: 9789811507267; 9811507260
• Notes: Note: Includes bibliographical references.
• Access Rights: Legal Deposit; Only available on premises controlled by the deposit library and to one user at any one time; The Legal Deposit Libraries (Non-Print Works) Regulations (UK).
• Access Usage: Restricted: Printing from this resource is governed by The Legal Deposit Libraries (Non-Print Works) Regulations (UK) and UK copyright law currently in force.