Optimizing Exhaust Nozzle/Airframe Thrust Minus Drag Grumman Aircraft Engineering Corporation

Format:

Conference/Event

Author/Creator:

Migdal, David, author.

Conference Name:

National Air Transportation Meeting (1968-04-29 : New York, New York, United States)

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1968

Summary:

This paper discusses exhaust nozzle performance, the interaction of exhaust nozzle and airframe, and the need for considering the effect of interactions when estimating overall performance. New performance parameters such as interference drag and equivalent thrust are introduced to account for these interactions. These parameters can be used to provide a consistent semi-empirical approach to optimizing exhaust nozzle/airframe performance and to measure achievements during the optimization process. Emphirical correlations based on the new parameters are displayed for several exhaust nozzle/aircraft combinations

Notes:

Vendor supplied data

Publisher Number:

680294

Access Restriction:

Restricted for use by site license