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Aerodynamics Supersonic
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Turbojet engines

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Online Results (32)
1.
Performance and surge limits of a TF30-P-3 turbofan engine/axisymmetric mixed-compression inlet propulsion system at Mach 2.5
Author
Wasserbauer, Joseph F.
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
2.
Mechanical characteristics of stability-bleed valves for a supersonic inlet
Author
Neiner, George H.
Published
Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
3.
Analysis of the dynamic response of a supersonic inlet to flow-field perturbations upstream of the normal shock
Author
Cole, Gary L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
4.
Analysis of the dynamic response of a supersonic inlet to flow-field perturbations upstream of the normal shock
Author
Cole, Gary L.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TN D-7839
Format
Books
5.
Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction
Author
Wasserbauer, Joseph F.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
6.
Design of a very-low-bleed Mach 2.5 mixed-compression inlet with 45 percent internal contraction
Author
Wasserbauer, Joseph F.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TM X-3135
Format
Books
7.
Effect of afterburner lights and inlet unstarts on a mixed-compression-inlet turbofan engine operating at Mach 2.5
Author
Baumbick, Robert J.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
8.
Effect of afterburner lights and inlet unstarts on a mixed-compression-inlet turbofan engine operating at Mach 2.5
Author
Baumbick, Robert J.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TM X-3223
Format
Books
9.
Evaluation by step response tests of prototype relief valves designed for YF-12 inlet stability bleed system
Author
Dustin, Miles O.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
10.
Evaluation by step response tests of prototype relief valves designed for YF-12 inlet stability bleed system
Author
Dustin, Miles O.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TM X-3262
Format
Books
11.
Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets
Author
Hingst, Warren R.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
12.
Evaluation of some control-volume techniques for analysis of shock-boundary-layer interactions in supersonic inlets
Author
Hingst, Warren R.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TM X-3186
Format
Books
13.
Experimental evaluation of a Mach 3.5 axisymmetric inlet
Author
Syberg, J.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
14.
Experimental evaluation of a Mach 3.5 axisymmetric inlet
Author
Syberg, J.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]
Location
Library Shelving Facility (LSF) >> NASA CR-2563
Format
Books
15.
Experimental investigation of a simple distortion index utilizing steady-state and dynamic distortions in a Mach 2.5 mixed-compression inlet and turbofan engine
Author
Costakis, William G.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
16.
Experimental investigation of a simple distortion index utilizing steady-state and dynamic distortions in a Mach 2.5 mixed-compression inlet and turbofan engine
Author
Costakis, William G.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TM X-3169
Format
Books
17.
Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet
Author
Neumann, Harvey E.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
18.
Performance of vortex generators in a Mach 2.5 low-bleed full-scale 45-percent-internal-contraction axisymmetric inlet
Author
Neumann, Harvey E.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Location
Library Shelving Facility (LSF) >> NASA TM X-3195
Format
Books
19.
Control system design using frequency domain models and parameter optimization, with application to supersonic inlet controls
Author
Seidel, Robert C.
Published
Washington, D.C., National Aeronautics and Space Administration, 1974.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
20.
Control system design using frequency domain models and parameter optimization, with application to supersonic inlet controls
Author
Seidel, Robert C.
Published
Washington, D.C., National Aeronautics and Space Administration, 1974.
Location
Library Shelving Facility (LSF) >> NASA TM X-3108
Format
Books
21.
Digital integrated control of a Mach 2.5 mixed-compression supersonic inlet and an augmented mixed-flow turbofan engine
Author
Batterton, Peter G.
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TM X-3075
Format
Books
22.
Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction
Author
Shaw, Robert J. (Robert Joseph), 1946-
Published
Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
23.
Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction
Author
Shaw, Robert J. (Robert Joseph), 1946-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TM X-2975
Format
Books
24.
Distributed porous throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60 percent internal contraction
Author
Shaw, Robert J. (Robert Joseph), 1946-
Published
Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1974.
Online
Online book
Location
HathiTrust Digital Library >> Online Resource
Format
Books / Online
25.
Distributed porous throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction
Author
Shaw, Robert J. (Robert Joseph), 1946-
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974.
Location
Library Shelving Facility (LSF) >> NASA TM X-2974
Format
Books