Optimization and performance analysis of a supersonic conical-flow waverider for a deck-launched intercept mission
Approved for public release; distribution is unlimited. === An aircraft configuration for a deck launched intercept mission was investigated. The mission requirements for the carrier-launched and recovered aircraft included Mach 6 cruise out to a 1000 nautical mile combat radius and 20 minutes of co...
Main Author: | Price, David R. |
---|---|
Other Authors: | Newberry, Conrad F. |
Language: | en_US |
Published: |
Monterey, California. Naval Postgraduate School
2014
|
Online Access: | http://hdl.handle.net/10945/39832 |
Similar Items
-
On waverider shapes applied to future supersonic and hypersonic configuration
by: 劉台安
Published: (1990) -
Supersonic flow field visualization studies of the MÅ = 6 price waverider planform
by: Garcia, Karl
Published: (2012) -
Experimental results of a Mach 10 conical-flow derived waverider to 14-X hypersonic aerospace vehicle
by: Tiago Cavalcanti Rolim, et al.
Published: (2011-05-01) -
The characteristics of waverider
by: LI, ZHENG-YUN, et al.
Published: (1988) -
Optimization and performance analysis of waverider configured interplanetary space vehicles
by: Flynn, John M.
Published: (2013)