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1) 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

2) Acoustic characteristics of a large-scale augmentor wing model at forward speed

Author

Falarski, Michael D

Series

NASA technical memorandum volume X-2940

Publisher

National Aeronautics and Space Administration

Pub. Date

November 1973.

Language

English

Formats

Book, Online Content

3) An overview of the quiet short-haul research aircraft program

Author

Shovlin, Michael D

Series

NASA technical memorandum volume 78545

Publisher

National Aeronautics and Space Administration

Pub. Date

November 1978.

Language

English

Formats

Book, Online Content

4) V/STOL model fan rig, design report

Author

Cheatham, J. G

Series

NASA contractor report volume NASA CR-174688

Publisher

National Aeronautics and Space Administration

Pub. Date

[1983]

Language

English

Formats

Book, Online Content

5) Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover

Author

Franklin, James A

Series

NASA technical memorandum volume 110399

Publisher

National Aeronautics and Space Administration, Ames Research Center

Pub. Date

June 1996.

Language

English

Formats

Book, Online Content

6) V/STOL concepts in the the United States: past, present, and future

Author

Nelms, W. P

Series

NASA technical memorandum volume 85938

Publisher

National Aeronautics and Space Administration, Ames Research Center

Pub. Date

[1984]

Language

English

Formats

Microfilm, Online Content

7) Analysis of internal flow in a ventral nozzle for STOVL aircraft

Author

Smith, C. Frederic

Series

NASA technical memorandum volume 103123

Publisher

For sale by the National Technical Information Service

Pub. Date

1990]

Language

English

Formats

Microfilm, Online Content

8) Research on a two-dimensional inlet for a supersonic V/STOL propulsion system

Author

Mark, J. L

Series

NASA contractor report volume NASA CR-174945

Publisher

National Aeronautics and Space Administration, Lewis Research Center

Pub. Date

[1989]

Language

English

Formats

Microfilm, Online Content

9) Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques

Author

Garg, Sanjay

Series

NASA technical memorandum volume 104340

Publisher

Lewis Research Center

Pub. Date

1991]

Language

English

Formats

Microfilm, Online Content

10) V/STOL model fan rig, design report

Author

Cheatham, J. G

Series

NASA contractor report volume NASA CR-174688

Publisher

National Aeronautics and Space Administration

Pub. Date

[1983]

Language

English

11) Computer simulation of a pilot in V/STOL aircraft control loops: Appendix III.The adaptive control model of a pilot in V/STOL aircraft control loops

Author

Vogt, William G

Series

NASA contractor report volume NASA CR-186599

Publisher

NASA Lewis Research Center

Pub. Date

[1988]

Language

English

Formats

Microfilm, Online Content

12) Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover

Author

Franklin, James A

Series

NASA technical memorandum volume 110399

Publisher

National Aeronautics and Space Administration, Ames Research Center

Pub. Date

[1996]

Language

English

13) Supersonic flow computations for an ASTOVL aircraft configuration: phase 2, part 2

Author

Ramakrishnan, Sekaripuram

Series

NASA contractor report volume NASA CR-4284

Publisher

National Aeronautics and Space Administration, Scientific and Technical Information Branch

Pub. Date

1990

Language

English

Formats

Microfilm, Online Content

14) Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles

Author

Kao, H. C

Publisher

National Aeronautics and Space Administration

Pub. Date

1984]

Language

English

15) Computer simulation of a pilot in V/STOL aircraft control loops: Appendix II.The optimal control model of a pilot in V/STOL aircraft control loops

Author

Vogt, William G

Series

NASA contractor report volume NASA CR-186598

Publisher

NASA Lewis Research Center

Pub. Date

[1989]

Language

English

Formats

Microfilm, Online Content

16) Flight propulsion control integration for V/STOL aircraft

Author

Mihaloew, James R

Publisher

NASA

Pub. Date

[1987]

Language

English

17) A flight-test methodology for identification of an aerodynamic model for a V/STOL aircraft

Author

Bach, Ralph E

Series

NASA technical memorandum volume 100067

Publisher

National Aeronautics and Space Administration, Ames Research Center

Pub. Date

[1988]

Language

English

Formats

Microfilm, Online Content

18) Analytical study of blowing boundary-layer control for subsonic V/STOL inlets

Author

Hwang, Danny P

Publisher

National Aeronautics and Space Administration

Pub. Date

1984]

Language

English

19) Assessment of aerodynamic performance of V/STOL and STOVL fighter aircraft

Author

Nelms, W. P

Series

NASA technical memorandum volume 85937

Publisher

National Aeronautics and Space Administration, Ames Research Center

Pub. Date

[1984]

Language

English

Formats

Microfilm, Online Content

20) A modeling technique for STOVL ejector and volume dynamics

Author

Drummond, Colin K

Series

NASA technical memorandum volume 103167

Publisher

For sale by the National Technical Information Service

Pub. Date

1990]

Language

English

Formats

Microfilm, Online Content

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Catalog Search Results

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

2) Acoustic characteristics of a large-scale augmentor wing model at forward speed

3) An overview of the quiet short-haul research aircraft program

4) V/STOL model fan rig, design report

5) Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover

6) V/STOL concepts in the the United States: past, present, and future

7) Analysis of internal flow in a ventral nozzle for STOVL aircraft

8) Research on a two-dimensional inlet for a supersonic V/STOL propulsion system

9) Integrated flight/propulsion control design for a STOVL aircraft using H-infinity control design techniques

10) V/STOL model fan rig, design report

11) Computer simulation of a pilot in V/STOL aircraft control loops: Appendix III.The adaptive control model of a pilot in V/STOL aircraft control loops

12) Moving base simulation evaluation of translational rate command systems for STOVL aircraft in hover

13) Supersonic flow computations for an ASTOVL aircraft configuration: phase 2, part 2

14) Flow visualization and interpretation of visualization data for deflected thrust V/STOL nozzles

15) Computer simulation of a pilot in V/STOL aircraft control loops: Appendix II.The optimal control model of a pilot in V/STOL aircraft control loops

16) Flight propulsion control integration for V/STOL aircraft

17) A flight-test methodology for identification of an aerodynamic model for a V/STOL aircraft

18) Analytical study of blowing boundary-layer control for subsonic V/STOL inlets

19) Assessment of aerodynamic performance of V/STOL and STOVL fighter aircraft

20) A modeling technique for STOVL ejector and volume dynamics