I agree that this site is using cookies. You can find further informations here.
X
Reubush, David E
25  results:
Search for persons X
?
1

Pressure and heat-transfer investigation of a hypersonic co..:

Reubush, David E. ; Omar, M. Emmett
Journal of Aircraft.  27 (1990)  5 - p. 418-422 , 1990
Link: https://doi.org/10.2514/..
 
?
2

Flowfield investigation of a supercruise fighter model:

Reubush, David E. ; Bare, E. Ann ; Yaros, Steven F..
Journal of Aircraft.  22 (1985)  4 - p. 289-295 , 1985
Link: https://doi.org/10.2514/..
 
?
3

Effect of Over-the-Wing Nacelles on Wing-Body Aerodynamics:

Reubush, David E.
Journal of Aircraft.  16 (1979)  6 - p. 359-365 , 1979
Link: https://doi.org/10.2514/..
 
?
4

Reynolds Number Effects on Boattaildrag of Wing-Bodies:

Reubush, David E.
Journal of Aircraft.  14 (1977)  5 - p. 455-459 , 1977
Link: https://doi.org/10.2514/..
 
?
5

Effect of Reynolds Number on Boattail Drag:

Reubush, David E.
Journal of Aircraft.  13 (1976)  5 - p. 334-337 , 1976
Link: https://doi.org/10.2514/..
 
?
6

Flow field over the wing of a delta-wing fighter model with..:

Bare, E. Ann ; Haddad, Raymond C ; Reubush, David E.
http://hdl.handle.net/2027/uiug.30112106713495.  , 1992
Link: http://hdl.handle.net/20..
 
?
7

Static internal performance of a two-dimensional convergent..:

Bare, E. Ann ; Reubush, David E ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
http://hdl.handle.net/2027/uiug.30112106605816.  , 1987
Link: http://hdl.handle.net/20..
 
?
8

Effects of the installation and operation of jet-exhaust ya..:

Reubush, David E ; Berrier, Bobby L ; Langley Research Center
http://hdl.handle.net/2027/uiug.30112106606269.  , 1987
Link: http://hdl.handle.net/20..
 
?
9

Investigation of a supersonic cruise fighter model flow fie..:

Reubush, David E ; Bare, E. Ann ; Langley Research Center
http://hdl.handle.net/2027/uiug.30112105149832.  , 1985
Link: http://hdl.handle.net/20..
 
?
10

Effect of thrust vectoring and wing maneuver devices on tra..:

Capone, Francis J ; Reubush, David E ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
http://hdl.handle.net/2027/uiug.30112106670687.  , 1983
Link: http://hdl.handle.net/20..
 
?
11

Effects of varying podded nacelle-nozzle installations on t..:

Capone, Francis J ; Reubush, David E ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
http://hdl.handle.net/2027/uiug.30112106571117.  , 1983
Link: http://hdl.handle.net/20..
 
?
12

Effects of installation of F101 DFE exhaust nozzles on the ..:

Reubush, David E ; Carlson, John R ; Langley Research Center.
http://hdl.handle.net/2027/uiug.30112005560609.  , 1982
Link: http://hdl.handle.net/20..
 
?
13

An experimental and theoretical investigation of the effect..:

Reubush, David E ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
http://hdl.handle.net/2027/uiug.30112106725697.  , 1979
Link: http://hdl.handle.net/20..
 
?
14

Effect of several airframe/nozzle modifications on the drag..:

Re, Richard J ; Reubush, David E ; Langley Research Center.
http://hdl.handle.net/2027/uiug.30112105097395.  , 1979
Link: http://hdl.handle.net/20..
 
?
15

Investigation of very low blockage ratio boattail models in..:

Reubush, David E ; United States. National Aeronautics and Space Administration
http://hdl.handle.net/2027/uiug.30112106917310.  , 1976
Link: http://hdl.handle.net/20..
 
1-15