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T. A. Reyhner
Observed names:
Reyhner, Theodore A.,
T. REYHNER,
T.A. Reyhner,
THEODORE A. REYHNER
Institution:
Boeing (United States)
Observed institutions:
Boeing (United States),
Stanford University
OpenAlex ID:
A5036847350
The interaction of a shock wave with a laminar boundary layer†
1968
·
T.A. Reyhner
, I. Flügge-Lotz
·
International Journal of Non-Linear Mechanics
·
270
Combined Viscous-Inviscid Analysis of Supersonic Inlet Flowfields
1972
·
THEODORE A. REYHNER
, TIMOTHY E. HICKCOX
·
Journal of Aircraft
·
31
Transonic Potential Flow Computation about Three-Dimensional Inlets, Ducts, and Bodies
1981
·
T. A. Reyhner
·
AIAA Journal
·
20
Cartesian Mesh Solution for Axisymmetric Transonic Potential Flow Around Inlets
1977
·
T. A. Reyhner
·
AIAA Journal
·
20
Transonic Potential Flow around Axisymmetric Inlets and Bodies at Angle of Attack
1977
·
T. A. Reyhner
·
AIAA Journal
·
19
Multigrid Code for Three-Dimensional Transonic Potential Flow about Inlets
1982
·
D. R. McCarthy
, T. A. Reyhner
·
AIAA Journal
·
14
Computation of transonic potential flow about 3 dimensional inlets, ducts, and bodies
1982
·
T. A. Reyhner
·
NASA STI Repository (National Aeronautics and Space Administration)
·
6
PDF
Transonic potential flow computation about three-dimensional inlets,ducts and bodies
1980
·
T. REYHNER
·
AIAA Fluid Dynamics, Plasma Dynamics and Lasers Conference
·
4
Three-dimensional transonic potential flow about complex 3-dimensional configurations
1984
·
T. A. Reyhner
·
NASA STI Repository (National Aeronautics and Space Administration)
·
3
PDF
A multi-grid code for 3-D transonic potential flow about axisymmetric inlets at angle of attack
1980
·
D. MCCARTHY
, T. REYHNER
·
AIAA Fluid Dynamics, Plasma Dynamics and Lasers Conference
·
3
Cartesian mesh solution for axisymmetric transonic potential flow around inlets
1976
·
T. REYHNER
·
AIAA Fluid Dynamics, Plasma Dynamics and Lasers Conference
·
3
A procedure for combined viscous-inviscid analysis of supersonic inlet flow fields
1972
·
T. REYHNER
, T. HICKCOX
·
10th Aerospace Sciences Meeting
·
3
Transonic potential flow around axisymmetric inlets and bodies at angle of attack
1977
·
T. REYHNER
·
15th Aerospace Sciences Meeting
·
2
Dynamic control of the WIND CFD code
2002
·
L.P. Wesley
, R.E. Childs
, et al.
·
IEEE Aerospace Conference (AERO)
·
1
A numerical method for 3D boundary layers with a small crossflow
1991
·
J. LEE
, G. PAYNTER
, et al.
·
AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Subsonic Propulsion System Installation Analysis and Optimization
1991
·
J. L. Colehour
, B. W. Farquhar
, et al.
·
Volume 2: Aircraft Engine; Marine; Microturbines and Small Turbomachinery
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Works count:
18
Citation count:
399
H-index:
6
I10-index:
6
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