-
1
-
-
84894600058
-
-
US Patent 3,905,566, 09/16/75
-
Anderson, Edwin R., US Patent 3,905,566, "Jet Engine Intake Protection System," 09/16/75.
-
Jet Engine Intake Protection System
-
-
Anderson, E.R.1
-
5
-
-
10244272918
-
-
NASA Research Grant NGL 43-001-086 Final Report, N74-35194, September
-
Bissinger, Norbert C., and Braun, Gerhard W., "On the Inlet Vortex System," NASA Research Grant NGL 43-001-086 Final Report, N74-35194, September 1974.
-
(1974)
On the Inlet Vortex System
-
-
Bissinger, N.C.1
Braun, G.W.2
-
6
-
-
82555179102
-
-
AIAA Paper No. 2000-3998
-
Brix, S., Neuwerth, G., Jacob, D., "The Inlet-Vortex System of Jet Engines Operating Near The Ground," AIAA Paper No. 2000-3998, 2000.
-
(2000)
The Inlet-Vortex System of Jet Engines Operating Near the Ground
-
-
Brix, S.1
Neuwerth, G.2
Jacob, D.3
-
7
-
-
0014982478
-
Inlet Vortex
-
January
-
Colehour, J.L. and Farquhar, B.W., "Inlet Vortex," Journal of Aircraft, Vol. 8, No. 1, pp39-43, January 1971.
-
(1971)
Journal of Aircraft
, vol.8
, Issue.1
, pp. 39-43
-
-
Colehour, J.L.1
Farquhar, B.W.2
-
8
-
-
84894582293
-
-
US Patent 3,474,988, 10/28/69
-
Cox, Peter Oliver, et al, US Patent 3,474,988, "Pod for a Gas Turbine Engine," 10/28/69.
-
Pod For a Gas Turbine Engine
-
-
Cox, P.O.1
-
9
-
-
0020203618
-
Mechanisms of Inlet-Vortex Formation
-
(Massachusetts Institute of Technology)
-
De Siervi, F., Viguier, H.C., Greitzer, E.M., and Tan, C.S., "Mechanisms of Inlet-Vortex Formation," J. Fluid Mechanics, 1982, Vol. 124, pp. 173-207 (Massachusetts Institute of Technology).
-
(1982)
J. Fluid Mechanics
, vol.124
, pp. 173-207
-
-
de Siervi, F.1
Viguier, H.C.2
Greitzer, E.M.3
Tan, C.S.4
-
11
-
-
0018532216
-
The Static Pressure in a Vortex Core
-
October
-
Dunham, J., "The Static Pressure in a Vortex Core," Aeronautical Journal Paper No. 623, October 1979.
-
(1979)
Aeronautical Journal Paper No
, pp. 623
-
-
Dunham, J.1
-
12
-
-
84894591764
-
-
US Patent 3,387,456, 06/11/68
-
Feder, Aaron, and Lavi, Rahim, US Patent 3,387,456, "Aerodynamic Shield Device for VTOL Jet Aircraft Engine Exhaust," 06/11/68.
-
Aerodynamic Shield Device For VTOL Jet Aircraft Engine Exhaust
-
-
Feder, A.1
Lavi, R.2
-
14
-
-
85067319397
-
-
AIAA Paper No. 2001-2449, June
-
Funk, R., Parekh, D., Smith, D., Dorris, J. "Inlet Vortex Alleviation," AIAA Paper No. 2001-2449, June 2001.
-
(2001)
Inlet Vortex Alleviation
-
-
Funk, R.1
Parekh, D.2
Smith, D.3
Dorris, J.4
-
18
-
-
84890140866
-
-
US Patent 2,915,262, 12/01/59
-
Klein, Harold J., US Patent 2,915,262, "Vortex Inhibitor for Aircraft Jet Engines," 12/01/59.
-
Vortex Inhibitor For Aircraft Jet Engines
-
-
Klein, H.J.1
-
20
-
-
84894593390
-
-
US Patent 3,298,637, 01/17/67
-
Lee, Shao-Tang, US Patent 3,298,637, "Engine Inlet Protective Screen Arrangement," 01/17/67.
-
Engine Inlet Protective Screen Arrangement
-
-
Shao-Tang, L.1
-
21
-
-
0022045026
-
Surface Static Pressures in an Inlet Vortex Flow Field
-
April, Massachusetts Institute of Technology)
-
Liu, W., Greitzer, E.M., and Tan, C.S., "Surface Static Pressures in an Inlet Vortex Flow Field," Journal of Engineering for Gas Turbines and Power, Vol. 107, pp. 387-393, April 1985 (Massachusetts Institute of Technology).
-
(1985)
Journal of Engineering For Gas Turbines and Power
, vol.107
, pp. 387-393
-
-
Liu, W.1
Greitzer, E.M.2
Tan, C.S.3
-
22
-
-
0015142019
-
Boeing 737 Engine Gravel Protection
-
October
-
Loughney, Charles E., "Boeing 737 Engine Gravel Protection," Journal of Aircraft, Vol. 8, No. 10, pp 792-795, October 1971.
-
(1971)
Journal of Aircraft
, vol.8
, Issue.10
, pp. 792-795
-
-
Loughney, C.E.1
-
23
-
-
85003211663
-
-
NASA-CR-62078, April
-
Mason, W.H. and Marchman, J.F., III, "Farfield Structure of an Aircraft Trailing Vortex, Including Effects of Mass Injection," NASA-CR-62078, April 1972.
-
(1972)
Farfield Structure of An Aircraft Trailing Vortex, Including Effects of Mass Injection
-
-
Mason, W.H.1
Marchman III, J.F.2
-
25
-
-
85040275049
-
-
Technical Note KTH AERO TN 62, Royal Institute Of Technology, Stockholm, Sweden)
-
Ridder, S.-O., and Samuelsson, I., "An Experimental Study of Strength and Existence Domain of Ground-to-Air Inlet Vortices by Ground Board Static Pressure Measurements," Technical Note KTH AERO TN 62, 1982 (Royal Institute Of Technology, Stockholm, Sweden).
-
(1982)
An Experimental Study of Strength and Existence Domain of Ground-to-Air Inlet Vortices By Ground Board Static Pressure Measurements
-
-
Ridder, S.-O.1
Samuelsson, I.2
-
28
-
-
84894526909
-
-
MIT Industrial Liaison Program Publication
-
Shin, H.W., Greitzer, E.M., Cheng, W.K., Tan, C.S. and Shippee, C.L., "Circulation Measurements and Vortical Structure in an Inlet Vortex Flow Field," MIT Industrial Liaison Program Publication, 1985.
-
(1985)
Circulation Measurements and Vortical Structure In An Inlet Vortex Flow Field
-
-
Shin, H.W.1
Greitzer, E.M.2
Cheng, W.K.3
Tan, C.S.4
Shippee, C.L.5
-
29
-
-
33845387358
-
-
III, US Patent 6,129,309, 10/10/00
-
Smith, David M. and Dorris, John, III, US Patent 6,129,309, "Aircraft Engine Apparatus With Reduced Inlet Vortex," 10/10/00.
-
Aircraft Engine Apparatus With Reduced Inlet Vortex
-
-
Smith, D.M.1
Dorris, J.2
-
30
-
-
77950582503
-
-
US Patent 3,527,430, 09/08/70
-
Smith, John Phillip, US Patent 3,527,430, "Protective Air Curtains for Aircraft Engine Inlets," 09/08/70.
-
Protective Air Curtains For Aircraft Engine Inlets
-
-
Smith, J.P.1
-
31
-
-
0016004686
-
Vortex Formation Near the Intakes to TurboMachinery and Duct Systems
-
Swainston, M.J.C., "Vortex Formation Near the Intakes to TurboMachinery and Duct Systems," Proc Instn Mech Engrs Vol 188, pp 597-605, 1974.
-
(1974)
Proc Instn Mech Engrs
, vol.188
, pp. 597-605
-
-
Swainston, M.J.C.1
-
32
-
-
84894580709
-
-
US Patent 4,070,827, 01/31/78
-
Vanfleet Charles R. and Ruehr William C., US Patent 4,070,827, "Method and Apparatus for Limiting Ingestion of Debris into the Inlet of a Gas Turbine Engine", 01/31/78.
-
Method and Apparatus For Limiting Ingestion of Debris Into the Inlet of a Gas Turbine Engine
-
-
Vanfleet, C.R.1
Ruehr, W.C.2
|