Aircraft thermal management : integrated energy system analysis / by Mark F. Ahlers.

Format:

Book

Author/Creator:

Ahlers, Mark F., author.

Contributor:

Society of Automotive Engineers, publisher.

Series:

Society of Automotive Engineers. Electronic publications.

PT ; 178

Society of Automotive Engineers. Electronic publications

PT (Series) (Warrendale, Pa.) ; 178.

Language:

English

Subjects (All):

Aerodynamic heating.

Aerothermodynamics.

Physical Description:

1 online resource (1 PDF (v, 109 pages)) : illustrations (some color), maps, charts (graphs, tables), plans.

Place of Publication:

Warrendale, Pennsylvania (400 Commonwealth Dr., Warrendale PA USA) : Society of Automotive Engineers, 2016.

Summary:

The simultaneous operation of all systems generating, moving, or removing heat on an aircraft is simulated using integrated analysis which is called Integrated Energy System Analysis (IESA) for this book. The purpose of this analytical modeling is to understand, optimize, and validate more efficient system architectures for removing or harvesting the increasing amounts of waste heat generated in commercial and military aircraft. In the commercial aircraft industry IESA is driven by the desire to minimize airplane operating costs associated with increased system weight, power consumption, drag, and lost revenue as cargo space is devoted to expanded cooling systems. In military aircraft thermal IESA is also considered to be a key enabler for the successful implementation of the next-generation jet fighter weapons systems and countermeasures.

Contents:

1. An exergy-based methodology for decision-based design of integrated aircraft thermal systems (2000-01-5527) / Figliola, R., and Tipton, R.

2. Dynamic thermal management system modeling of a more electric aircraft (2008-01-2886) / McCarthy, K., Walters, E., Heltzel, A., Elangovan, R., et. al.

3. Facilitating the energy optimization of aircraft propulsion and thermal management systems through integrated modeling and simulation (2010-01-1787) / Maser, A., Garcia, E., and Mavris, D.

4. Power thermal management system design for enhanced performance in an aircraft vehicle (2010-01-1805) / Bodie, M.

5. Integrated electrical and thermal management sub-system optimization (2010-01-1812) / Bodden, D., Eller, B., and Clements, S.

6. Thermal management investigations for fuel cell systems on-board commercial aircraft (2013-01-2274) / Vredenborg, E., and Thielecke, F.

7. Advantages of the dynamic simulation for the thermal management systems design (2014-01-2152) / Del Valle, P., and Blazquez Munoz, P.

8. A thermal management assessment tool for advanced hypersonic aircraft (921941) / Issacci, F., Wassel, A. Farr, J., Wallace, C., et al.

9. Model-based thermal management functions for aircraft systems (2014-01-2203) / Schlabe, D., and Lienig, J.

10. A modeling approach for integrated thermal management system analysis of aircraft (971242) / Van Griethuysen, V.J., Issacci, F., and Farr, J., Jr.

Notes:

Includes bibliographical references.

Description based on print version record.

ISBN:

0-7680-8727-9

0-7680-8304-4

1-5231-0632-8

OCLC:

957454455