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1) Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities

Author

Leavitt, Laurence D

Series

NASA technical paper volume 2519

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch

Pub. Date

1985

Language

English

Formats

Book, Online Content

2) Preliminary experiments on the noise generated by target-type thrust reverser models

Author

Gutierrez, Orlando A

Series

NASA technical memorandum volume X-2553

Publisher

National Aeronautics and Space Administration

Pub. Date

May 1972.

Language

English

Formats

Book, Online Content

3) Plasma actuators for turbomachinery flow control, final report

Author

Miles, Richard B

Series

NASA contractor report volume NASA CR-217654

Publisher

National Aeronautics and Space Administration, Glenn Research Center

Pub. Date

[2012]

Language

English

Formats

Book, Online Content

4) An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner

Author

Arbiter, Dorothy G

Series

NASA contractor report volume NASA CR-178036

Publisher

National Aeronautics and Space Administration, Langley Research Center

Pub. Date

[1985]

Language

English

Formats

Book, Online Content

5) Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers

Author

Green, Robert S

Series

NASA technical memorandum volume 89044

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch

Pub. Date

1987

Language

English

Formats

Book, Online Content

6) Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap

Author

Re, Richard J

Series

NASA technical paper volume 2549

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch

Pub. Date

April 1986.

Language

English

Formats

Book, Online Content

7) Static performance of six innovative thrust reverser concepts for subsonic transport applications: summary of the NASA Langley Innovative Thrust Reverser Test Program

Author

Asbury, Scott C

Series

NASA technical memorandum volume 2000-210300

Publisher

National Aeronautics and Space Administration, Langley Research Center

Pub. Date

July 2000.

Language

English

Formats

Book, Online Content

8) Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers

Author

Green, Robert S

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch

Pub. Date

1987

Language

English

Formats

Microfilm, Online Content

9) Static performance of six innovative thrust reverser concepts for subsonic transport applications: summary of the NASA Langley Innovative Thrust Reverser Test Program

Author

Asbury, Scott C

Series

NASA technical memorandum volume 2000-210300

Publisher

National Aeronautics and Space Administration, Langley Research Center

Pub. Date

[2000]

Language

English

Formats

Microfilm, Online Content

10) An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner

Author

Arbiter, Dorothy G

Series

NASA contractor report volume NASA CR-178036

Publisher

National Aeronautics and Space Administration, Langley Research Center

Pub. Date

[1985]

Language

English

11) Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability

Author

Bangert, Linda S

Series

NASA technical paper volume 2933

Publisher

National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division

Pub. Date

1989

Language

English

Formats

Microfilm, Online Content

12) Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap

Author

Re, Richard J

Series

NASA technical paper volume 2549

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch

Pub. Date

1986

Language

English

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Catalog Search Results

1) Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities

2) Preliminary experiments on the noise generated by target-type thrust reverser models

3) Plasma actuators for turbomachinery flow control, final report

4) An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner

5) Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers

6) Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap

7) Static performance of six innovative thrust reverser concepts for subsonic transport applications: summary of the NASA Langley Innovative Thrust Reverser Test Program

8) Measured pressure distributions inside nonaxisymmetric nozzles with partially deployed thrust reversers

9) Static performance of six innovative thrust reverser concepts for subsonic transport applications: summary of the NASA Langley Innovative Thrust Reverser Test Program

10) An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner

11) Static internal performance of a nonaxisymmetric vaned thrust reverser with flow splay capability

12) Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap