My Account Log in

3 options

Hypersonic technology for military application / Committee on Hypersonic Technology for Military Application, Air Force Studies Board, Commission on Engineering and Technical Systems, National Research Council.

EBSCOhost Academic eBook Collection (North America) Available online

View online

Ebook Central Academic Complete Available online

View online

National Academies Press Available online

View online
Format:
Book
Author/Creator:
National Research Council (U.S.) Committee on Hypersonic Technology for Military Application., Corporate Author.
Language:
English
Subjects (All):
Hypersonic planes.
Airplanes, Military.
Physical Description:
1 online resource (111 p.)
Edition:
1st ed.
Place of Publication:
Washington, D.C. : National Academy Press, 1989.
Language Note:
English
Contents:
Hypersonic Technology for Military Application
Copyright
Contents
Executive Summary
MILITARY APPLICATIONS
NATIONAL AEROSPACE PLANE PROGRAM
TECHNOLOGY ASSESSMENT
Propulsion-Airframe Integration
Propulsion Systems
Aerodynamics
Control, Guidance, and Information Systems
Materials, Structures, and Cooling
The Role of Computational Fluid Dynamics
Test Requirements
Introduction
1.0 Potential Military Hypersonic Applications
2.0 Technologies Relevant to Hypersonic Vehicles and Their Status
2.1 AERODYNAMIC-PROPULSIVE INTEGRATION
2.2 PROPULSION SYSTEMS
2.2.1 Basic Scramjet Engine
2.2.2 Cooling Problems
2.2.3 Propulsion System Transition
2.2.4 Auxiliary Rocket Propulsion
2.3 AERODYNAMICS
2.3.1 Viscous Effects
2.3.1.1 Transition Point Determination
2.3.1.2 Extent of the Transition Region
2.3.1.3 Turbulent Boundary Layer
2.3.1.4 Test Conditions
2.3.2 Real Gas Effects
2.3.3 Real Gas Effects in Complex Flows
2.4 CONTROL, GUIDANCE, INSTRUMENTATION, AND INFORMATION SYSTEMS
2.4.1 Physical Factors
2.4.2 Vehicle Dynamics and Controls
2.4.2.1 "Aerodynamic-Attitude" (Angle of Attack and Sideslip) Control
2.4.2.2 Integrated Propulsion/Flight Control and Guidance
2.4.2.3 Aerothermoelastic and Slosh Mode Characteristics and Control
2.4.2.4 Engine/Inlets/Diffuser, etc., Control
2.4.3 Sensors
2.4.4 Information System Requirements
2.4.5 System Design Philosophy
2.5 MATERIALS FOR HYPERSONIC VEHICLES
2.5.1 Introduction
2.5.2 High Temperature Materials
2.5.2.1 The Aluminides
2.5.2.2 Superalloys
2.5.2.3 Dispersion Strengthened (Stabilized) Alloys
2.5.2.4 Carbon-Carbon Composites And Ceramic Composite Materials
2.5.2.5 Processing Developments For Advanced Metallic Materials
2.5.2.6 Other Developments
2.5.3 Coatings.
2.6 THE STRUCTURAL CHALLENGE
2.6.1 Determination of Structural Mass Fraction for High Performance Vehicles
2.6.2 Structural Concepts
2.6.3 Development Process
2.6.4 Status of Structural Concepts for Hypersonic Vehicles
2.6.5 Structural Design Considerations
2.6.5.1 The Structural Designer's Approach, Circa 1988
2.6.5.2 The Aerodynamic Heating Phenomena
2.6.5.3 The Temperature Distribution in the Structure
2.6.5.4 Structural Effects of High Temperatures
2.6.5.5 Summary
2.7 ROLE OF COMPUTATIONAL FLUID DYNAMICS
2.7.1 Status of Hypersonic CFD
2.7.1.1 External Aerodynamics
2.7.1.2 Inlet Flows
2.7.1.3 Combustion Flows
2.7.1.4 Nozzle Flows
2.7.2 Validation of Hypersonic CFD Codes
2.7.3 Future Role of CFD
2.8 EXPERIMENTAL CAPABILITIES
2.8.1 Test Requirements
2.8.2 Aerodynamic Test Capabilities
2.8.3 Materials and Structures Test Facilities
2.8.3.1 Structures Testing
2.8.3.2 Facilities
2.8.3.3 High-Speed Wind Tunnel Tests
2.8.3.4 Laboratory Tests with Heating Devices
3.0 Findings and Recommendations
3.1 POTENTIAL MILITARY HYPERSONIC APPLICATIONS
3.2 PROPULSION-AIRFRAME INTEGRATION
3.3 PROPULSION SYSTEMS
3.4 AERODYNAMICS
3.4.1 Low Hypersonic Speeds (Mach Numbers 6 to 10)
3.4.2 High Hypersonic Speeds (M &gt
10)
3.5 CONTROLS, GUIDANCE, INSTRUMENTATION AND INFORMATION PROCESSING
3.6 HIGH TEMPERATURE MATERIALS, CRYOGENICS, AND COOLING
3.7 STRUCTURAL CONCEPTS
3.8 THE ROLE OF CFD
3.9 TEST REQUIREMENTS
Appendix A: Statement Of Task
Appendix B: Acronyms
Appendix C: Glossary
Appendix D: Dimensionless Groups In Fluid Mechanics
Appendix E: Letter To National Aerospace Plane Contractors
INTRODUCTION
BROAD ISSUES
TECHNOLOGICAL ISSUES
Hypersonic Propulsion
Low Speed Propulsion
Boundary Layer Transition
Vehicle Heating.
Structures and Materials
Control
Systems Integration
System Concept
Appendix F: Schedule of Committee Meetings
AGENDA
AGENDA.
Notes:
Bibliographic Level Mode of Issuance: Monograph
ISBN:
9786610212446
9781280212444
1280212446
9780309582551
0309582555
9780585144030
0585144036
OCLC:
70772757

The Penn Libraries is committed to describing library materials using current, accurate, and responsible language. If you discover outdated or inaccurate language, please fill out this feedback form to report it and suggest alternative language.

My Account

Shelf Request an item Bookmarks Fines and fees Settings

Guides

Using the Library Catalog Using Articles+ Library Account