Wind Tunnel Tests and Modeling Studies of Ice Accretion Relevant to Aircraft Engines.

Wind Tunnel Tests and Modeling Studies of Ice Accretion Relevant to Aircraft Engines.

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2003

Pub. Year:

2003

No.:

2003-0906

Paper no.:

2003-0906

Pages:

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001712
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	41st
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2003.01.06-2003.01.09
Note for article:	41st AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 6-9 January 2003

Similar Items:

1 Technical Paper Experimental Study of Ice Adhesion to Airfoils Relevant to Aircraft Engines. Venkataramani, K.S. American Institute of Aeronautics and Astronautics	7 Technical Paper Spectral Analysis and Experimental Modeling of Ice Accretion Roughness Orr, D. J., Breuer, K. S., Torres, B. E., Hansman, R. J., Jr. National Aeronautics and Space Adminstration
2 Technical Paper Aircraft Engine Icing Model K. Venkataramani, R. Plybon, R. Holm, B. Krupp American Institute of Aeronautics and Astronautics	8 Technical Paper Wind Tunnel Testing of the Wright Brothers Model B Airfoil Landman,D., Alvarez,J., Blackburn,S., Ash,R., Hyde,K. American Institute of Aeronautics and Astronautics
3 Technical Paper Spectral analysis and experimental modeling of ice accretion roughness Orr, D.J., Breuer, K.S., Torres, B.E., Hansman, R.J., Jr. American Institute of Aeronautics and Astronautics	9 Technical Paper Plans and Status of Wind-Tunnel Testing Employing an Aeroservoelastic Semispan Model B. Perry, W. Silva, J. Florance, C. Wieseman, A. Pototzky, M. Sanetrik, R. Scott, D. Keller, S. Cole, D. Coulson American Institute of Aeronautics and Astronautics
4 Technical Paper High speed shock impingement studies using innovative movement of model components to expedite testing in traditional wind tunnel facilities Neumann, R.D. American Institute of Aeronautics and Astronautics	10 Technical Paper A High Performance Aircraft Wind Tunnel Test Using Response Surface Methodologies Landman, D., Simpson, J., Mariani, R., Ortiz, F., Britcher, C. American Institute of Aeronautics and Astronautics
5 Technical Paper Dynamic Response Tests of Inertial and Optical Wind-Tunnel Model Attitude Measurement Devices Buehrle, R.D., Young, C.P., Jr., Burner, A.W., Tripp, J.S., Tcheng, P., Finley, T.D., Popernack, T.G., Jr. National Aeronautics and Space Adminstration	11 Technical Paper Wind Tunnel Testing of an Adaptive Control System for Vibration Suppression on Aircraft A. Wildschek, R. Maier, F. Hoffmann, J. Steigenberger, K. Kaulfuss, C. Breitsamter, A. Allen, N. Adams, H. Baier, T. … American Institute of Aeronautics and Astronautics
6 Technical Paper Hyper-X wind tunnel program McClinton, C.R., Holland, S.D., Rock, K.E., Engelund, W.C., Voland, R.T., Huebner, L.D., Rogers, R.C. American Institute of Aeronautics and Astronautics	12 Technical Paper The Effect on Aerodynamic Drag of the Longitudinal Position of a Road Vehicle Model in a Wind Tunnel Test Section Garry,K.P., Cooper,K.R., Fediw,A., Wallis,S.B., Wilsden,D.J. Society of Automotive Engineering, Inc.

1

2

3

4

5

6

7

8

9

10

11

12