ARAMA SONUÇLARI

Toplam 23 adet sonuçtan 20 tanesi görüntülenmektedir.

The effect of sweep angle on the limit cycle oscillations of aircraft wings

ADVANCES IN AIRCRAFT AND SPACECRAFT SCIENCE, Vol. 2, No. 2, Ocak 2015, s. 199-215, ISSN: 2287-528X

EKEN SEHER, KAYA METİN ORHAN

Internal Ballistic Modeling of a Solid Rocket Motor by Analytical Burnback Analysis

Journal of Spacecraft and Rockets, Vol. 56, No. 2, Mart 2019, s. 498-516, ISSN: 0022-4650

TOLA CEYHUN,NİKBAY MELİKE

Solid Rocket Motor Propellant Optimization with Coupled Internal Ballistic–Structural Interaction Approach

Journal of Spacecraft and Rockets, Vol. 55, No. 4, Temmuz 2018, s. 936-947, ISSN: 0022-4650

TOLA CEYHUN,NİKBAY MELİKE