ARAMA SONUÇLARI

Toplam 23 adet sonuçtan 20 tanesi görüntülenmektedir.

Investigation of the Effect of Thickness Taper Ratio and Aspect Ratio on Fin Flutter Velocity of a Model Rocket using Response Surface Method

7th International Conferenceon Recent Advances in Space Technologies, Istanbul/TÜRKİYE, 16 Haziran 2015

CEYHUN TOLA,NİKBAY MELİKE

Development of a Design and Performance Evaluation Code of Hybrid Rocket Motors

Asian Joint Conference on Propulsion and Power, 16 Mart 2016

COSKUNPINAR ERDİ,ÖZEN KAAN,GRATE STANISLAV,ASLAN ALİM RÜSTEM

Alim Rüstem Aslan Tam metin bildiri

Solid rocket motor design using a surrogate model

AIRCRAFT ENGINEERING AND AEROSPACE TECHNOLOGY, Vol. 90, No. 7, Ekim 2018, s. 1104-1127, ISSN: 1748-8842

TOLA CEYHUN,NİKBAY MELİKE

Melike Nikbay Özgün Makale