NDLI: F-15/nonaxisymmetric nozzle system integration study support program

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F-15/nonaxisymmetric nozzle system integration study support program

Content Provider	NASA Technical Reports Server (NTRS)
Author	Stevens, H. L.
Copyright Year	1978
Description	Nozzle and cooling methods were defined and analyzed to provide a viable system for demonstration 2-D nozzle technology on the F-15 aircraft. Two candidate cooling systems applied to each nozzle were evaluated. The F-100 engine mount and case modifications requirements were analyzed and the actuation and control system requirements for two dimensional nozzles were defined. Nozzle performance changes relative to the axisymmetric baseline nozzle were evaluated and performance and weight characteristics for axisymmetric reference configurations were estimated. The infrared radiation characteristics of these nozzles installed on the F-100 engine were predicted. A full scale development plan with associated costs to carry the F100 engine/two-dimensional (2-D) nozzle through flight tests was defined.
File Size	7122336
Page Count	169
File Format	PDF
Alternate Webpage(s)	http://archive.org/details/NASA_NTRS_Archive_19780010127
Archival Resource Key	ark:/13960/t8tb5x493
Language	English
Publisher Date	1978-02-01
Access Restriction	Open
Subject Keyword	Aircraft Propulsion And Power Nozzle Design Cooling Aerodynamic Configurations Engine Design Airframes Systems Engineering Nozzle Thrust Coefficients Thrust Reversal Aircraft Engines F-15 Aircraft Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science
Content Type	Text
Resource Type	Technical Report

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