C.M., N. S. (2017). The Effects of Tail-Tilt on the Yaw Stability of Baseline-V Blended Wing Body Aircraft / Nur Syazwani C.M and Rizal E.M. Nasir. Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM).
استشهاد بنمط شيكاغوC.M., Nur Syazwani. The Effects of Tail-Tilt On the Yaw Stability of Baseline-V Blended Wing Body Aircraft / Nur Syazwani C.M and Rizal E.M. Nasir. Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM), 2017.
MLA استشهادC.M., Nur Syazwani. The Effects of Tail-Tilt On the Yaw Stability of Baseline-V Blended Wing Body Aircraft / Nur Syazwani C.M and Rizal E.M. Nasir. Faculty of Mechanical Engineering Universiti Teknologi MARA (UiTM), 2017.
تحذير: قد لا تكون هذه الاستشهادات دائما دقيقة بنسبة 100%.