Class information for:
Level 1: AERODYNAM BRANCH//CONING MOTION//MISSILE SYST DAHLGREN

Basic class information

ID Publications Average number
of references
Avg. shr. active
ref. in WoS
20811 384 18.7 23%



Bar chart of Publication_year

Last years might be incomplete

Classes in level above (level 2)



ID, lev.
above
Publications Label for level above
429 15725 JOURNAL OF COMPUTATIONAL PHYSICS//INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS//COMPUTERS & FLUIDS

Terms with highest relevance score



Rank Term Type of term Relevance score
(tfidf)
Class's shr.
of term's tot.
occurrences
Shr. of publ.
in class containing
term
Num. of
publ. in
class
1 AERODYNAM BRANCH Address 21 65% 5% 20
2 CONING MOTION Author keyword 4 67% 1% 4
3 MISSILE SYST DAHLGREN Address 4 75% 1% 3
4 SPINNING MISSILE Author keyword 3 57% 1% 4
5 CATASTROPHIC YAW Author keyword 3 100% 1% 3
6 STEADY STATE SPIN Author keyword 3 100% 1% 3
7 GRID FIN Author keyword 3 60% 1% 3
8 RDRL WML E Address 2 67% 1% 2
9 BALLIST WE CONCEPTS WE MAT DIRECT Address 1 100% 1% 2
10 PRECISION MUNITION Author keyword 1 100% 1% 2

Web of Science journal categories

Author Key Words



Rank Web of Science journal category Relevance score
(tfidf)
Class's shr.
of term's tot.
occurrences
Shr. of publ.
in class containing
term
Num. of
publ.
in class
LCSH search Wikipedia search
1 CONING MOTION 4 67% 1% 4 Search CONING+MOTION Search CONING+MOTION
2 SPINNING MISSILE 3 57% 1% 4 Search SPINNING+MISSILE Search SPINNING+MISSILE
3 CATASTROPHIC YAW 3 100% 1% 3 Search CATASTROPHIC+YAW Search CATASTROPHIC+YAW
4 STEADY STATE SPIN 3 100% 1% 3 Search STEADY+STATE+SPIN Search STEADY+STATE+SPIN
5 GRID FIN 3 60% 1% 3 Search GRID+FIN Search GRID+FIN
6 PRECISION MUNITION 1 100% 1% 2 Search PRECISION+MUNITION Search PRECISION+MUNITION
7 WRAP AROUND FINS 1 50% 1% 2 Search WRAP+AROUND+FINS Search WRAP+AROUND+FINS
8 SET FORWARD 1 40% 1% 2 Search SET+FORWARD Search SET+FORWARD
9 SUPERSONIC FLIGHT 1 40% 1% 2 Search SUPERSONIC+FLIGHT Search SUPERSONIC+FLIGHT
10 AERODYNAMICS DATABASE 1 50% 0% 1 Search AERODYNAMICS+DATABASE Search AERODYNAMICS+DATABASE

Key Words Plus



Rank Web of Science journal category Relevance score
(tfidf)
Class's shr.
of term's tot.
occurrences
Shr. of publ.
in class containing
term
Num. of
publ. in
class
1 ATMOSPHERIC FLIGHT 23 100% 3% 10
2 CONTROL AUTHORITY 17 100% 2% 8
3 DUAL SPIN PROJECTILE 14 100% 2% 7
4 CONING MOTION 9 83% 1% 5
5 NAVIER STOKES PREDICTIONS 8 75% 2% 6
6 LATERAL PULSE JETS 3 100% 1% 3
7 SYMMETRIC MISSILE 3 100% 1% 3
8 ARTILLERY ROCKET 1 100% 1% 2
9 CANARD CONTROLLED MISSILE 1 100% 1% 2
10 DITHERING CANARDS 1 100% 1% 2

Journals

Reviews



Title Publ. year Cit. Active
references
% act. ref.
to same field
Catastrophic yaw. Why, what, how? 2013 1 6 100%
Review and extension of computational methods for noncircular cross-sectional weapons 1998 0 3 100%

Address terms



Rank Address term Relevance score
(tfidf)
Class's shr.
of term's tot.
occurrences
Shr. of publ.
in class containing
term
Num. of
publ. in
class
1 AERODYNAM BRANCH 21 65% 5.2% 20
2 MISSILE SYST DAHLGREN 4 75% 0.8% 3
3 RDRL WML E 2 67% 0.5% 2
4 BALLIST WE CONCEPTS WE MAT DIRECT 1 100% 0.5% 2
5 AEROSP TRANSPORTAT ADV SYST 1 25% 0.8% 3
6 BALLIST WE ONS CONCEPTS 1 50% 0.3% 1
7 EECN 1 50% 0.3% 1
8 INTERIOR BALLIST AEROBALLIST 1 50% 0.3% 1
9 MECH SYST ENGN GRP 1 50% 0.3% 1
10 MISSILES 1 50% 0.3% 1

Related classes at same level (level 1)



Rank Relatedness score Related classes
1 0.0000152691 FIELD BOUNDARY ELEMENTS//CHIMERA METHODOLOGY//HIGH SPEED AERODYNAMICS
2 0.0000131437 MISSILE GUIDANCE//GUIDANCE LAW//PROPORTIONAL NAVIGATION
3 0.0000092681 V WING//CONICAL FLOWS//VORTEX FERRI SINGULARITIES
4 0.0000088881 DELTA WING//HIGH ANGLE OF ATTACK//DOUBLE DELTA WING
5 0.0000068603 PARAGLIDER//INFLATABLE CELL MODEL//PK PARACHUTE GRP
6 0.0000067691 LAUNCH DYNAM//MARITIME POLICE SCI//TRANSFER STIFFNESS COEFFICIENT METHOD
7 0.0000067006 DYNAM SYST CONTROL BRANCH//AIRCRAFT PARAMETER ESTIMATION//FLIGHT DYNAM BRANCH
8 0.0000066007 COMPRESSIBLE TURBULENCE//SHOCKLET//COMPRESSIBLE MIXING LAYER
9 0.0000054815 OPPOSING JET//HYPERSONIC SHOCK TUNNEL//FORWARD FACING CAVITY
10 0.0000053431 DEV TEST//GRAIN DESIGN//SATELLITE LAUNCH VEHICLE