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GlNO MORETTI
Observed names:
G. MORETTI,
G. Moretti,
Moretti, G.
Observed institutions:
Northrop Grumman (United States),
Applied Science Laboratories (United States),
British Aerospace (United Kingdom),
Instituto Politécnico do Rio de Janeiro,
University of Salford,
Sapienza University of Rome,
SUNY Polytechnic Institute
show all 7
OpenAlex ID:
A5113536243
A time-dependent computational method for blunt body flows.
1966
·
GlNO MORETTI
, MlCHAEL ABBETT
·
AIAA Journal
·
233
A new technique for the numerical analysis of nonequilibrium flows
1965
·
GlNO MORETTI
·
AIAA Journal
·
108
Three-Dimensional Flow around Blunt Bodies
1967
·
GlNO MORETTI
, GARY BLEICH
·
AIAA Journal
·
62
A complete numerical technique for the calculation of three-dimensional inviscid supersonic flows
1972
·
G. MORETTI
, B. GROSSMAN
, et al.
·
10th Aerospace Sciences Meeting
·
40
Three-dimensional Supersonic Flow Computations
1963
·
GlNO MORETTI
·
AIAA Journal
·
40
Experimental analysis of thermal fields in horizontally eccentric cylindrical annuli
1992
·
G. Guj
, S. Iannetta
, et al.
·
Experiments in Fluids
·
34
Inviscid flowfield about a pointed cone at an angle of attack.
1967
·
GlNO MORETTI
·
AIAA Journal
·
29
A fast Euler solver for steady flows
1983
·
G. MORETTI
·
AIAA Computational Fluid Dynamics Conference
·
22
A physical approach to the numerical treatment of boundaries in gas dynamics
1981
·
G. Moretti
·
NASA Technical Reports Server (NASA)
·
22
Grid generation using classical techniques
1980
·
G. Moretti
·
NASA STI Repository (National Aeronautics and Space Administration)
·
20
PDF
Three-dimensional, supersonic, steady flows with any number of imbedded shocks
1974
·
G. MORETTI
·
12th Aerospace Sciences Meeting
·
20
Shock-boundary layer interaction by shock fitting
1993
·
G. Moretti
, F. Marconi
, et al.
·
Lecture notes in physics
·
18
Time-dependent computation of transonic flows
1970
·
B. GROSSMAN
, G. MORETTI
·
AIAA Annual Meeting and Technical Display
·
15
The blunt body problem for a viscous rarefied gas flow
1969
·
G. MORETTI
·
7th Aerospace Sciences Meeting
·
15
Numerical experiments on the leading edge flow field
1981
·
L. ZANNETTI
, G. MORETTI
·
AIAA Computational Fluid Dynamics Conference
·
14
An improved lambda-scheme for one-dimensional flows
1983
·
G. Moretti
, M. T. Dipiano
·
NASA STI Repository (National Aeronautics and Space Administration)
·
13
PDF
Analysis of two-dimensional problems of supersonic combustion controlled by mixing
1964
·
G. MORETTI
·
Aerospace Sciences Meeting
·
12
Muzzle Blast Flow and Related Problems
1978
·
G. MORETTI
·
AIAA Fluid Dynamics, Plasma Dynamics and Lasers Conference
·
10
A new, improved computational technique for two-dimensional, unsteady, compressible flows
1982
·
G. MORETTI
, L. ZANNETTI
·
20th Aerospace Sciences Meeting
·
9
Conformal mappings for computations of steady, three-dimensional, supersonic flows
1976
·
G. Moretti
·
NASA Technical Reports Server (NASA)
·
9
Aerodynamic technology — the role of aerodynamic technology in the design and development of modern combat aircraft
1996
·
T. McMichael
, K. McKay
, et al.
·
The Aeronautical Journal
·
5
Calculation of three-dimensional, inviscid, supersonic, steady flows
1981
·
G. Moretti
·
NASA STI Repository (National Aeronautics and Space Administration)
·
5
PDF
A circumspect exploration of a difficult feature of multidimensional imbedded shocks
1975
·
G. Moretti
·
5
Inviscid Flow Field Past a Pointed Cone at an Angle of Attack. Part 1 - Analysis
1965
·
G. Moretti
·
Defense Technical Information Center (DTIC)
·
5
Development of analytical methods of predicting the pressure distribution about a nacelle at transonic speeds: Exact solution
1973
·
B. Grossman
, G. Moretti
·
NASA Technical Reports Server (NASA)
·
4
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Works count:
50
Citation count:
790
H-index:
14
I10-index:
18
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