1-24 of 109 Books

High Temperature Electronics Design for Aero Engine Controls and Health Monitoring
By Lucian Stoica,Steve Riches,Colin Johnston
Jet aircraft engines
Jet aircraft engines
By Irwin E. Treager

The development of jet and turbine aero engines
By Bill Gunston
Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot
Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot
By A. G. Powell
Jet-engine fundamentals
Jet-engine fundamentals
By Norman E. Borden
WINCOF-I code for prediction of fan compressor unit with water ingestion
WINCOF-I code for prediction of fan compressor unit with water ingestion
By S. N. B. Murthy

La propulsione a reazione in Italia dalle origini al 1943
By Giuseppe Ciampaglia
Continued development of expert system tools for NPSS engine diagnostics
Continued development of expert system tools for NPSS engine diagnostics
By Henry Lewandowski

Ersten Strahlflugzeuge der Welt
By Wagner, Wolfgang
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets
By Charles J. Trefny
Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [sic, i.e. 2.0]
Tests with a two-dimensional intake having all-external compression and a design mach number of 2.2 [sic, i.e. 2.0]
By M. C. Neale

Military Jet Engine Acquistion
By Obaid Younossi

Elements of gas turbine propulsion
By Jack D. Mattingly
Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
Theoretical flow characteristics of inlets for tilting-nacelle VTOL aircraft
By Michael A. Boles
The "Apollo" of aeronautics
The "Apollo" of aeronautics
By Mark D. Bowles
The jet race and the Second World War
The jet race and the Second World War
By Sterling Michael Pavelec

The Care And Maintenance Of Heavy Jets
By Christian Parker
Noise suppression with high Mach number inlets
Noise suppression with high Mach number inlets
By Edward Lumsdaine