E-LIB Suche - Ergebnisse für: Bare, E. Ann

1

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/..

2

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..

3

Static internal performance of convergent single-expansion-..:

Bare, E. Ann ; Capone, Francis J
http://hdl.handle.net/2027/uiug.30112106724112. , 1989

Link: http://hdl.handle.net/20..

4

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..

5

Multiaxis control power from thrust vectoring for a superso..:

Capone, Francis J ; Bare, E. Ann ; Langley Research Center
http://hdl.handle.net/2027/uiug.30112106605725. , 1987

Link: http://hdl.handle.net/20..

6

Effect of a trade between boattail angle and wedge size on ..:

Carson, George T ; Burley, James R ; Bare, E. Ann.
http://hdl.handle.net/2027/uiug.30112106605766. , 1987

Link: http://hdl.handle.net/20..

7

Aerodynamic characteristics of a supersonic fighter aircraf..:

Capone, Francis J ; Arbiter, Dorothy ; Bare, E. Ann.
http://hdl.handle.net/2027/uiug.30112106613968. , 1986

Link: http://hdl.handle.net/20..

8

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..

9

Effect of thrust reverser operation on the lateral-directio..:

Bare, E. Ann ; Pendergraft, Odis C ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
http://hdl.handle.net/2027/uiug.30112105146440. , 1983

Link: http://hdl.handle.net/20..

10

Effects of twin-vertical-tail parameters on twin-engine aft..:

Leavitt, Laurence D ; Bare, E. Ann ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
http://hdl.handle.net/2027/uiug.30112106673731. , 1983

Link: http://hdl.handle.net/20..

11

Investigation of installation effects on twin-engine conver..:

Bare, E. Ann ; Berrier, Bobby L ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
http://hdl.handle.net/2027/uiug.30112105146671. , 1983

Link: http://hdl.handle.net/20..

12

Effect of nozzle and vertical-tail variables on the perform..:

Pendergraft, Odis C ; Bare, E. Ann ; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
http://hdl.handle.net/2027/uiug.30112101593454. , 1982

Link: http://hdl.handle.net/20..

13

Effect of in-flight thrust reversing on vertical-tail loads..:

Bare, E. Ann ; Capone, Francis J ; Berrier, Bobby L..
http://hdl.handle.net/2027/uiug.30112106670901. , 1981

Link: http://hdl.handle.net/20..

14

Inducible hepatic expression of CREBH mitigates diet-induce..:

Krumm, Christopher S. ; Xu, Xu ; Bare, Curtis J....
Journal of Biological Chemistry. 297 (2021) 1 - p. 100815 , 2021

Link: https://doi.org/10.1016/..

15

Novel Signal Transduction Pathway Utilized by Extracellular..:

Asea, Alexzander ; Rehli, Michael ; Kabingu, Edith...
Journal of Biological Chemistry. 277 (2002) 17 - p. 15028-15034 , 2002

Link: https://doi.org/10.1074/..