|
|
|
|
|
Michele Ferlauto, Andrea Ferrero, Matteo Marsicovetere and Roberto Marsilio
Aerospike nozzles represent an interesting solution for Single-Stage-To-Orbit or clustered launchers owing to their self-adapting capability, which can lead to better performance compared to classical nozzles. Furthermore, they can provide thrust vectori...
ver más
|
|
|
|
|
|
|
|
|
|
|
Hidemi Takahashi, Toshihiko Munakata and Shigeru Sato
The airframe-integrated linear-spike nozzle concept applied to an external nozzle for high-speed aircraft was evaluated with regard to the thrust augmentation capability and the trim balance. The main focus was on the vehicle aftbody. The baseline airfra...
ver más
|
|
|
|
|
|
|
|
|
|
|
Hidemi Takahashi
A practical approach for deriving the absolute density field based on the background-oriented schlieren method in a high-speed flowfield was implemented. The flowfield of interest was a two-dimensional compressible flowfield created by two supersonic str...
ver más
|
|
|
|
|
|