Effects of Fuel-nozzle Carbon Deposition on Combustion Efficiency of Single Tubular-type, Reverse-flow Turbojet Combustor at Simulated Altitude Conditions PDF Download
Are you looking for read ebook online? Search for your book and save it on your Kindle device, PC, phones or tablets. Download Effects of Fuel-nozzle Carbon Deposition on Combustion Efficiency of Single Tubular-type, Reverse-flow Turbojet Combustor at Simulated Altitude Conditions PDF full book. Access full book title Effects of Fuel-nozzle Carbon Deposition on Combustion Efficiency of Single Tubular-type, Reverse-flow Turbojet Combustor at Simulated Altitude Conditions by Ralph T. Dittrich. Download full books in PDF and EPUB format.
Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Carbon
Languages : en
Pages : 34
Get Book Here
Book Description
A study was made to determine the cause of irreproducibility of combustion data of a single tubular-type turbojet combustor operating at simulated altitude conditions.
Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Carbon
Languages : en
Pages : 34
Get Book Here
Book Description
A study was made to determine the cause of irreproducibility of combustion data of a single tubular-type turbojet combustor operating at simulated altitude conditions.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 388
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 774
Get Book Here
Book Description
Author: Warren A. Tucker
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 738
Get Book Here
Book Description
A theoretical analysis, based on the linearized equation for supersonic flow, of characteristics of triangular-tip control surfaces on thin triangular wings. By restriction to case for which Mach lines from wing apex lie behind the leading edge, a simplified treatment was possible; results of previous work on lift of triangular wings could be used to derive expressions for lift effectiveness, pitching moment, rolling-moment effectiveness, hinge moment due to control deflection, and hinge moment due to angle of attack. Comparisons were made with two-dimensional case.
Author:
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 528
Get Book Here
Book Description
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 666
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1620
Get Book Here
Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 90
Get Book Here
Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aeronautical Research and Development
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 542
Get Book Here
Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Get Book Here
Book Description
