2) Static performance of a fixed-geometry exhaust nozzle incorporating porous cavities for shock-boundary layer interaction control

Author
Asbury, Scott C
Series
NASA technical memorandum volume 1999-209513
Publisher
National Aeronautics and Space Administration, Langley Research Center
Pub. Date
August 1999.
Language
English

3) Separate flow nozzle test status meeting: proceedings of a conference held at and sponsored by NASA Glenn Research Center, Cleveland, Ohio, September 9-10, 1997

Series
NASA conference publication volume 210524
Publisher
National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
Pub. Date
[2000]
Language
English

4) Shelf life extension for the lot AAE nozzle severance LSCs: final test report

Author
Cook, M
Series
NASA contractor report volume NASA CR-183878
Publisher
Thiokol Corp., Space Operations
Pub. Date
1990]
Language
English

5) Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model

Author
Castner, Raymond
Series
NASA technical memorandum volume 2012-217446
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
[2012]
Language
English

6) Analysis and design of optimized truncated scarfed nozzles subject to external flow effects

Author
Shyne, Rickey J
Publisher
For sale by the National Technical Information Service
Pub. Date
1990]
Language
English

7) Noise from aft deck exhaust nozzles: differences in experimental embodiments

Author
Bridges, James E
Series
NASA technical memorandum volume 2014-218123
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
April 2014.
Language
English

8) Derivation of the data reduction equations for the calibration of the six-component thrust stand in the CE-22 advanced nozzle test facility

Author
Wong, Kin C
Series
NASA technical memorandum volume 212326
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
2003]
Language
English

9) Experimental investigation of an ejector-powered free-jet facility

Author
Long, Mary Jo
Series
NASA technical memorandum volume 105868
Publisher
National Aeronautics and Space Administration
Pub. Date
1992]
Language
English

10) A comparison of combustor-noise models

Author
Hultgren, Lennart S
Series
NASA technical memorandum volume 2012-217671
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
2012.
Language
English

11) Exhaust nozzle plume effects on sonic boom test results for vectored nozzles

Author
Castner, Raymond S
Series
NASA technical memorandum volume 217229
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
[2012]
Language
English

12) Exhaust nozzle plume effects on sonic boom test results for isolated nozzles

Author
Castner, Raymond S
Series
NASA technical memorandum volume 217137
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
[2011]
Language
English

13) Jet noise reduction potential from emerging variable cycle technologies

Author
Henderson, Brenda S
Series
NASA technical memorandum volume 217744
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
[2012]
Language
English

14) Slot nozzle effects for reduced sonic boom on a generic supersonic wing section

Author
Castner, Raymond S
Series
NASA technical memorandum volume 216258
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
[2010]
Language
English

15) Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet

Author
Ponton, Michael K
Series
NASA technical memorandum volume 1999-209336
Publisher
National Aeronautics and Space Administration, Langley Research Center
Pub. Date
May 1999.
Language
English

16) Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft

Author
Esker, Barbara S
Publisher
For sale by the National Technical Information Service
Pub. Date
1990]
Language
English

18) Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles

Author
Castner, Raymond S
Series
NASA technical memorandum volume 216259
Publisher
National Aeronautics and Space Administration, Glenn Research Center
Pub. Date
[2010]
Language
English

19) Experimental and analytical study of close-coupled ventral nozzles for ASTOVL aircraft

Author
McArdle, Jack G
Publisher
For sale by the National Technical Information Service
Pub. Date
1990]
Language
English