Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components

Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components PDF Author: Carl E. Campbell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

Get Book Here

Book Description
Compressor performance and turbine performance are presented in the form of performance maps at selected values of Reynolds number index; the effects of Reynolds number on performance are summarized. The effects of variable stator angle and high inlet-air temperatures on compressor performance are also shown. Over-all engine performance (net thrust and specific fuel consumption) is presented for a flight Mach number of 0.9 at rated engine conditions over a range of altitudes to illustrate performance losses resulting from decreased Reynolds number index.

Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components

Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components PDF Author: Carl E. Campbell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

Get Book Here

Book Description
Compressor performance and turbine performance are presented in the form of performance maps at selected values of Reynolds number index; the effects of Reynolds number on performance are summarized. The effects of variable stator angle and high inlet-air temperatures on compressor performance are also shown. Over-all engine performance (net thrust and specific fuel consumption) is presented for a flight Mach number of 0.9 at rated engine conditions over a range of altitudes to illustrate performance losses resulting from decreased Reynolds number index.

Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components

Performance of Basic XJ79-GE-1 Turbojet Engine and Its Components PDF Author: Carl E. Campbell
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 62

Get Book Here

Book Description
Compressor performance and turbine performance are presented in the form of performance maps at selected values of Reynolds number index; the effects of Reynolds number on performance are summarized. The effects of variable stator angle and high inlet-air temperatures on compressor performance are also shown. Over-all engine performance (net thrust and specific fuel consumption) is presented for a flight Mach number of 0.9 at rated engine conditions over a range of altitudes to illustrate performance losses resulting from decreased Reynolds number index.

NACA Research Memorandum

NACA Research Memorandum PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 80

Get Book Here

Book Description


NASA Technical Memorandum

NASA Technical Memorandum PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 946

Get Book Here

Book Description


Index to NASA Technical Publications

Index to NASA Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages :

Get Book Here

Book Description


A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 450

Get Book Here

Book Description


Index of N A S A Technical Publications

Index of N A S A Technical Publications PDF Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category :
Languages : en
Pages : 448

Get Book Here

Book Description


U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 178

Get Book Here

Book Description


XJ79-GE-13 Turbojet Engine

XJ79-GE-13 Turbojet Engine PDF Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages :

Get Book Here

Book Description


Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1766

Get Book Here

Book Description