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100   $a20030701d2002      uy         0
101 0 $aeng
135   $aurcn|||||||||
181   $ctxt
182   $cc
183   $acr
200 00$aAdvanced hypersonic test facilities /$fedited by Frank Lu, Dan Marren
205   $a1st ed.
210   $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$dc2002
215   $a1 online resource (646 p.)
225 1 $aProgress in astronautics and aeronautics ;$vv. 198
300   $aDescription based upon print version of record.
311 08$a1-56347-541-3 
320   $aIncludes bibliographical references and index.
327   $a""Cover""; ""Title""; ""Copyright""; ""Table of Contents""; ""Preface""; ""Chapter 1 Hypersonic Ground Test Requirements""; ""I. Introduction""; ""II. History, Status, and Outlook for Hypersonic Test Requirements""; ""III. Potential Civilian Hypersonic Test Requirements Futures""; ""A. Planetary Exploration""; ""B. Access to Space""; ""IV. Military Hypersonic Test Requirements Futures""; ""A. Access to Space""; ""B. Missiles""; ""V. Conclusion""; ""References""; ""Chapter 2 Principles of Hypersonic Test Facility Development""; ""I. Introduction""; ""II. Critical Hypersonic Technologies""
327   $a""III. Hypersonic Scaling""""IV. High Enthalpy and High Speed""; ""V. Types of Hypersonic Facilities""; ""VI. Conclusions""; ""Acknowledgments""; ""References""; ""Chapter 3 NASA's HYPULSE Facility at GASL A Dual Mode, Dual Driver Reflected-Shock/Expansion Tunnel""; ""I. Introduction""; ""A. Background""; ""B. Scope of the Chapter""; ""II. Shock Tunnels and Expansion Tubes""; ""A. Shock-Heated Facilities""; ""B. Reflected-Shock Tunnels""; ""C. Shock-Expansion Tubes""; ""III. Driver Methods""; ""A. Lighter Gases""; ""B. Electrically Heated Light Gases""
327   $a""C. Combustion Heated Light Gases""""D. Compressively Heated Light Gases (Free-Piston Driver)""; ""E. Summary of Comparison of Driver Techniques""; ""F. The Shock-Induced Detonation Driver for HYPULSE""; ""IV. Operation and Performance of HYPULSE""; ""A. Facility Configuration and Sizing""; ""B. HYPULSE Operation""; ""C. Test Conditions Verification""; ""D. Test Time Determination""; ""V. Driver Gas Contamination in Detonation-Driven RST Mode""; ""A. Nozzle Flow""; ""B. Transient Development of Driver-Gas Leakage""; ""VI. Nozzle Design for Expansion Tunnel Mode Operation""
327   $a""A. Skimmer Nozzles""""B. Full Capture Contoured Inlet Asymptoting to a Conical Profile""; ""C. Verification with Experiments""; ""VII. Concluding Remarks""; ""Acknowledgments""; ""References""; ""Chapter 4 LENS Hypervelocity Tunnels and Application to Vehicle Testing at Duplicated Flight Conditions""; ""I. Introduction""; ""II. Ground Test Simulation of Hypersonic Flight Performance""; ""III. Design, Operation, and Performance of the LENS I and LENS II Hypervelocity Ground Test Facilities""; ""A. Introduction""; ""B. Design and Operation of the LENS I and II Shock Tunnels""
327   $a""C. Aerothermal, Aero-Optic, and Radiation Instrumentation Suites""""IV. Facility Validation""; ""V. Application of Test Facility and Instrumentation to Hypersonic Vehicle Testing""; ""A. Evaluation of the Aerothermal and Aero-optical Characteristics of High-Speed Interceptors""; ""B. Examples of Aerothermal Measurements to Evaluate Seekerhead Performance""; ""C. Example of Aero-Optic Measurements on Interceptor Seekerhead Configurations""; ""VI. Measurements of Jet Interaction Resulting from Divert Thruster Operation""; ""A. Introduction""; ""B. Flowfield and Aerothermal Characteristics""
327   $a""C. Spectrometer and Radiometer Measurements of Flowfield Obscuration Phenomena""
330   $aWith the technical challenges that simulations of Mach 5-plus speeds pose for wind tunnel ground testing facilities, such testing has been characterized as "the art of partial simulation." Lu (mechanical and aerospace engineering, U. of Texas at Arlington) and Marren (Arnold Engineering Development Center, White Oak, MD) introduce 22 contributed chapters expanding the knowledge base on developments in hypersonic facilities in the past decade by focusing on testing principles; specific types of facilities (e.g., NASA's HYPULSE, LENS hypervelocity tunnels, and the U-12 large shock tube); and innovations including new instrumentation capabilities, advances in material sciences, and increasing international cooperation. Readers are referred elsewhere for treatment of perfect gas wind tunnels. Annotation copyrighted by Book News, Inc., Portland, OR
410  0$aProgress in astronautics and aeronautics ;$vv. 198.
606   $aAerodynamics, Hypersonic
606   $aHypersonic wind tunnels
606   $aBallistic ranges
606   $aRocket sleds
615  0$aAerodynamics, Hypersonic.
615  0$aHypersonic wind tunnels.
615  0$aBallistic ranges.
615  0$aRocket sleds.
676   $a629.132306
701   $aLu$b Frank K$0101202
701   $aMarren$b Dan E$01863306
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910971123903321
996   $aAdvanced hypersonic test facilities$94469879
997   $aUNINA