An investigation of tailored upstream heating for sonic boom and drag reduction

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Marconi, Frank ^a  

^a NORTHROP GRUMMAN CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; DRAG; DRAG REDUCTION; FIGHTER AIRCRAFT; HEATING; SHOCK WAVES; VEHICLES;

ATMOSPHERIC HEATING; COMPUTATIONAL RESULTS; HEATING DISTRIBUTIONS; ON-BOARD SYSTEMS; POWER REQUIREMENT; SONIC-BOOM ALLEVIATION; SUPERSONIC SPEED; VEHICLE SURFACE;

SUPERSONIC AIRCRAFT;

EID: 84982318025     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (7)

1. McLean, E., "Configuration Design for Specific Pressure Signaturè Characteristics," NASA SP-180, 1968.
2. Miller, D. S., and Carlson, H. W., "A Study of the Application of Heat or Force Field to the Sonic-Boom-Minimization Problem," NASA TND-5582, 1969.
3. Miller, D. S., and Carlson, H. W., "On the Application of Heat or Force Field to the Sonic-Boom-Minimization Problem," AIAA Paper 70-903, 1970.
4. Batdorf, S. B., "On Alleviation of the Sonic Boom by Thermal Means," AIAA Paper 701323.
5. Cheng, S., and Goldburg, A., "An Analysis of the Possibility of Reduction of Sonic Boom by Elector-Aerodynamic Devices," Boeing Scientific Research Lab. Report, D1-82-0764.
6. Selby, J., private communication.
7. Tretyakov, P. K., Garamin, A. F., Kraynev, V. L., Tupikin, A. V., and Yakovfev, V. I., "Investigation of Local Laser Energy Release Influence on Supersonic Flow by Methods of Aerophysical Experiments," Institute of Theoretical and Applied Mechanics SB RAS, Novosibirsk, Russia, 1996.