Variable Cycle Engine Evaluations for Supersonic V/STOL Fighters. Management Summary Report

Variable Cycle Engine Evaluations for Supersonic V/STOL Fighters. Management Summary Report PDF Author: J. E. Cupstid
Publisher:
ISBN:
Category :
Languages : en
Pages : 58

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Book Description
Variable cycle engines (VCE) have been evaluated using advanced V/STOL fighter designs. The VCE payoffs were assessed in terms of total weapon system cost effectiveness and results indicate that they offer potential benefits in supersonic V/STOL fighters. A systematic engine/airframe evaluation procedure was developed and used to assess interactions for advanced engine concepts in L + L/C aircraft designs. The evaluation procedure provides a rapid and inexpensive technique for evaluating engine concepts considering a large matrix of engine and airframe design and sizing variables. The procedure was used to establish a parametric data base using both fixed cycle turbofans and variable geometry turbine turbojets. Specific engine/airframe designs were then selected for detailed comparisons. Engine/airframe design evaluations were also conducted using a variable cycle turbofan engine capable of being used with both L + L/C and L/C aircraft. These aircraft designs were compared to the fixed cycle turbofan and variable geometry turbine turbojet aircraft designs in terms of TOGW, performance, life cycle cost and operational flexibility. (Author).

Variable Cycle Engine Evaluations for Supersonic V/STOL Fighters. Management Summary Report

Variable Cycle Engine Evaluations for Supersonic V/STOL Fighters. Management Summary Report PDF Author: J. E. Cupstid
Publisher:
ISBN:
Category :
Languages : en
Pages : 58

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Book Description
Variable cycle engines (VCE) have been evaluated using advanced V/STOL fighter designs. The VCE payoffs were assessed in terms of total weapon system cost effectiveness and results indicate that they offer potential benefits in supersonic V/STOL fighters. A systematic engine/airframe evaluation procedure was developed and used to assess interactions for advanced engine concepts in L + L/C aircraft designs. The evaluation procedure provides a rapid and inexpensive technique for evaluating engine concepts considering a large matrix of engine and airframe design and sizing variables. The procedure was used to establish a parametric data base using both fixed cycle turbofans and variable geometry turbine turbojets. Specific engine/airframe designs were then selected for detailed comparisons. Engine/airframe design evaluations were also conducted using a variable cycle turbofan engine capable of being used with both L + L/C and L/C aircraft. These aircraft designs were compared to the fixed cycle turbofan and variable geometry turbine turbojet aircraft designs in terms of TOGW, performance, life cycle cost and operational flexibility. (Author).

Variable Cycle Engine Evaluations for Supersonic V/STOL Fighters. Phase II and III Technical Report

Variable Cycle Engine Evaluations for Supersonic V/STOL Fighters. Phase II and III Technical Report PDF Author: J. E. Cupstid
Publisher:
ISBN:
Category :
Languages : en
Pages : 153

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Book Description
Variable cycle engines (VCE) have been evaluated using advanced V/STOL fighter designs. The VCE payoffs were assessed in terms of total weapon system cost effectiveness and results indicate that they offer potential benefits in supersonic V/STOL fighters. A systematic engine/airframe evaluation procedure was developed and used to assess interactions for advanced engine concepts in L + L/C aircraft designs. The evaluation procedure provdies a rapid and inexpensive technique for evaluating engine concepts considering a large matrix for engine and airframe design and sizing variables. The procedure was used to establish a parametric data base using both fixed cycle turbofans and variable geometry turbine turbojets. Specific engine/airframe designs were then selected for detailed comparisons. Engine/airframe design evaluations were also conducted using a variable cycle turbofan engine capable of being used with both L + L/C and L/C aircraft. These aircraft designs were compared to the fixed cycle turbofan and variable geometry turbine turbojet aircraft designs in terms of TOGW, performance, life cycle cost and operational flexibility. (Author).

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1572

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NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580

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Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 524

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A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).

Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
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ISBN:
Category : Science
Languages : en
Pages : 1108

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Government reports annual index

Government reports annual index PDF Author:
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ISBN:
Category :
Languages : en
Pages : 1190

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Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
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ISBN:
Category : Science
Languages : en
Pages :

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Aeronautical Engineering: A Cumulative Index to the 1984 Issues of the Continuing Bibliography

Aeronautical Engineering: A Cumulative Index to the 1984 Issues of the Continuing Bibliography PDF Author:
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ISBN:
Category :
Languages : en
Pages : 582

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Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 235)

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 235) PDF Author:
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ISBN:
Category :
Languages : en
Pages : 492

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