Browsing by Author ANANTHKRISHNAN, N

Jump to: 0-9 A B C D E F G H I J K L M N O P Q R S T U V W X Y Z
or enter first few letters:  
Showing results 1 to 20 of 26  next >
Issue DateTitleAuthor(s)
2005Aircraft spin recovery, with and without thrust vectoring, using nonlinear dynamic inversionRAGHAVENDRA, PK; SAHAI, T; KUMAR, PA; CHAUHAN, M; ANANTHKRISHNAN, N
1998Application of secondary bifurcations to large-amplitude limit cycles in mechanical systemsANANTHKRISHNAN, N; SUDHAKAR, K; SUDERSHAN, S; AGARWAL, A
2004Approximate analytical criterion for aircraft wing rock onsetANANTHKRISHNAN, N; SHAH, P; UNNIKRISHNAN, S
2000Bifurcation analysis for onset and cessation of surge in axial flow compressorsAGARWAL, A; ANANTHKRISHNAN, N
2003Bifurcation analysis of inertia coupled roll manoeuvres of airplanesSINHA, NK; ANANTHKRISHNAN, N
1996Characterization of periodic motions in aircraft lateral dynamicsANANTHKRISHNAN, N; SUDHAKAR, K
2000Comment On "Does The Phugoid Frequency Depend On Speed?"ANANTHKRISHNAN, N
2003Comments on "literal approximations to aircraft dynamics modes" and "consistent approximations to aircraft longitudinal modes" - replyANANTHKRISHNAN, N; RAMADEVI, P
2002Consistent approximations to aircraft longitudinal modesANANTHKRISHNAN, N; RAMADEVI, P
2009Design and development of a novel 2DOF actuation Slosh RigGANDHI, PS; JOSHI, KB; ANANTHKRISHNAN, N
2006Development of 2DOF actuation slosh rig : a novel mechatronic systemGANDHI, PS; MOHAN, J; JOSHI, KB; ANANTHKRISHNAN, N
2003Global stability and control analysis of axial compressor stall and surge phenomena using bifurcation methodsANANTHKRISHNAN, N; VAIDYA, UG; WALIMBE, VW
1995Inertia-coupled coordinated roll maneuvers of airplanesANANTHKRISHNAN, N; SUDHAKAR, K
1996Jump phenomena in Y-shaped intake ductsSUDHAKAR, K; ANANTHKRISHNAN, N
2000Large-amplitude limit cycles in resonantly coupled oscillatorsANANTHKRISHNAN, N; SUDERSHAN, S; SUDHAKAR, K; VERMA, A
2000Large-amplitude limit cycles via a homoclinic bifurcation mechanismSHARMA, A; ANANTHKRISHNAN, N
2001Level flight trim and stability analysis using extended bifurcation and continuation procedureANANTHKRISHNAN, N; SINHA, NK
2001Literal approximations to aircraft dynamic modesANANTHKRISHNAN, N; UNNIKRISHNAN, S
2002Maximum steady roll rate in zero-sideslip roll maneuvers of aircraftSINHA, NK; ANANTHKRISHNAN, N
1998Multiple attractors in inertia-coupled velocity-vector roll maneuvers of airplanesMODI, A; ANANTHKRISHNAN, N