|
 | Up a level |
Hameed, AS and Bindu, GR and Vutukuri, S (2024) Approach and landing guidance using constrained model predictive static programming. In: Aerospace Science and Technology, 144 .
Ghosh, A and Rao, SMV (2024) Development of maximum conical shock angle limit for osculating cone waveriders. In: Aerospace Science and Technology, 147 .
Suryanarayana, GK and Singh, DB and Surya, Sumukh and Jagadeesh, G (2022) Nonlinear damping model for supersonic air-intake buzz. In: Aerospace Science and Technology, 126 (107567). ISSN 12709638
Pattnaik, SPS and Rajan, NKS (2022) Numerical investigation of impact of fixed-exit boundary-layer bleed on supersonic intake performance. In: Aerospace Science and Technology, 120 .
Devaraj, MKK and Jutur, P and Rao, SMV and Jagadeesh, G and Anavardham, GTK (2021) Investigation of local unstart in a hypersonic scramjet intake at a Mach number of 6. In: Aerospace Science and Technology, 115 .
Kumar, SS and Bhanudasji Alone, D and Thimmaiah, SM and Mudipalli, JRR and Kumar, L and Ganguli, R and Kandagal, SB and Jana, S (2021) Aerodynamic behavior of a transonic axial flow compressor stage with self-recirculating casing treatment. In: Aerospace Science and Technology, 112 .
Rao, SMV and Karthick, SK (2019) Studies on the effect of imaging parameters on dynamic mode decomposition of time-resolved schlieren flow images. In: Aerospace Science and Technology, 88 . pp. 136-146.
Kumar, SS and Bhanudasji Alone, D and Thimmaiah, SM and Mudipalli, JRR and Ganguli, R and Kandagal, SB and Jana, S (2018) Aerodynamic characterization of a transonic axial flow compressor stage – with asymmetric tip clearance effects. In: Aerospace Science and Technology, 82-83 . pp. 272-283.
Chawla, Charu and Sarmah, P and Padhi, Radhakant (2010) Suboptimal reentry guidance of a reusable launch vehicle using pitch plane maneuver. In: Aerospace Science and Technology, 14 (6). pp. 377-386.
Viswamurthy, Sathyamangalam Ramanarayanan and Ganguli, Ranjan (2004) An optimization approach to vibration reduction in helicopter rotors with multiple active trailing edge flaps. In: Aerospace Science and Technology, 8 (3). pp. 185-194.
Suresh, S and Omkar, SN and Mani, V and Prakash, Guru TN (2003) Lift coefficient prediction at high angle of attack using recurrent neural network. In: Aerospace Science and Technology, 7 (8). pp. 595-602.
