Author: S-16 Turbine Engine Inlet Flow Distortion Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This document reviews the state of the art for data scaling issues associated with air induction system development for turbine-engine-powered aircraft. In particular, the document addresses issues with obtaining high quality aerodynamic data when testing inlets. These data are used in performance and inlet-engine compatibility analyses. Examples of such data are: inlet recovery, inlet turbulence, and steady-state and dynamic total-pressure inlet distortion indices. Achieving full-scale inlet/engine compatibility requires a deep understanding of three areas: 1) geometric scaling fidelity (referred to here as just "scaling"), 2) impact of Reynolds number, and 3) ground and flight-test techniques (including relevant environment simulation, data acquisition, and data reduction practices). The Model-to-Full Scale Subcommittee of the S-16 Turbine Engine Inlet Flow Distortion Committee has examined archives and has obtained recollections of experts regarding air induction system development experience to produce this document. The intent of this document is to capture the experience and lessons learned since approximately 1967 necessary to ensure that model-scale inlet total-pressure recovery and distortion data faithfully represent the corresponding full-scale inlet recovery and distortion characteristics.This document contains information that is fundamental to the discipline of inlet-engine compatibility and is expected to remain stable for the foreseeable future.
Inlet/Engine Compatibility - From Model to Full Scale Development
Results of a Full-scale B-1 Inlet/engine Compatibility Test at Subsonic and Supersonic Mach Numbers
Author: H. E. McDill
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 416
Book Description
Publisher:
ISBN:
Category : Jet engines
Languages : en
Pages : 416
Book Description
Results of the Full-scale F-15 Inlet/engine Compatibility Test at Subsonic and Supersonic Mach Numbers
Author: H. E. McDill
Publisher:
ISBN:
Category : Eagle (Jet fighter plane)
Languages : en
Pages : 330
Book Description
Publisher:
ISBN:
Category : Eagle (Jet fighter plane)
Languages : en
Pages : 330
Book Description
Inlet
Author: S-16 Turbine Engine Inlet Flow Distortion Committee
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This document reviews the state of the art for data scaling issues associated with air induction system development for turbine-engine-powered aircraft. In particular, the document addresses issues with obtaining high quality aerodynamic data when testing inlets. These data are used in performance and inlet-engine compatibility analyses. Examples of such data are: inlet recovery, inlet turbulence, and steady-state and dynamic total-pressure inlet distortion indices. Achieving full-scale inlet/engine compatibility requires a deep understanding of three areas: 1) geometric scaling fidelity (referred to here as just "scaling"), 2) impact of Reynolds number, and 3) ground and flight-test techniques (including relevant environment simulation, data acquisition, and data reduction practices). The Model-to-Full Scale Subcommittee of the S-16 Turbine Engine Inlet Flow Distortion Committee has examined archives and has obtained recollections of experts regarding air induction system development experience to produce this document. The intent of this document is to capture the experience and lessons learned since approximately 1967 necessary to ensure that model-scale inlet total-pressure recovery and distortion data faithfully represent the corresponding full-scale inlet recovery and distortion characteristics.
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
Book Description
This document reviews the state of the art for data scaling issues associated with air induction system development for turbine-engine-powered aircraft. In particular, the document addresses issues with obtaining high quality aerodynamic data when testing inlets. These data are used in performance and inlet-engine compatibility analyses. Examples of such data are: inlet recovery, inlet turbulence, and steady-state and dynamic total-pressure inlet distortion indices. Achieving full-scale inlet/engine compatibility requires a deep understanding of three areas: 1) geometric scaling fidelity (referred to here as just "scaling"), 2) impact of Reynolds number, and 3) ground and flight-test techniques (including relevant environment simulation, data acquisition, and data reduction practices). The Model-to-Full Scale Subcommittee of the S-16 Turbine Engine Inlet Flow Distortion Committee has examined archives and has obtained recollections of experts regarding air induction system development experience to produce this document. The intent of this document is to capture the experience and lessons learned since approximately 1967 necessary to ensure that model-scale inlet total-pressure recovery and distortion data faithfully represent the corresponding full-scale inlet recovery and distortion characteristics.
Technical Abstract Bulletin
Advanced Tactical Fighter to F-22 Raptor
Author: David C. Aronstein
Publisher: AIAA
ISBN: 9781600867903
Category : F-22 (Jet fighter plane)
Languages : en
Pages : 332
Book Description
Publisher: AIAA
ISBN: 9781600867903
Category : F-22 (Jet fighter plane)
Languages : en
Pages : 332
Book Description
Results of the Full-scale F-15 Inlet/engine Compatibility Test at Subsonic and Supersonic Mach Numbers
Author: H. E. McDill
Publisher:
ISBN:
Category : Eagle (Jet fighter plane).
Languages : en
Pages : 0
Book Description
Publisher:
ISBN:
Category : Eagle (Jet fighter plane).
Languages : en
Pages : 0
Book Description
Scientific and Technical Aerospace Reports
Fiscal Year 1975 Authorization for Military Procurement, Research, and Development, and Active Duty, Selected Reserve and Civilian Personnel Strengths
Author: United States. Congress. Senate. Committee on Armed Services
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 740
Book Description
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 740
Book Description
The Aerothermodynamics of Aircraft Gas Turbine Engines
Author: Gordon C. Oates
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 830
Book Description
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 830
Book Description