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Collection of Technical Papers - AIAA Applied Aerodynamics Conference

Volumn 1, Issue , 2004, Pages 92-111

Studies of combined use of CFD and wind tunnel test approaches to simulate a store separation from F-15E using efficient CFD database generation

(5) Lee, Jae M a Dunworth, Kevin S a Rizk, Magdi a Westmoreland, William S a Atkins, Donald J a

a AIR FORCE RESEARCH LABORATORY (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; COMPUTER SIMULATION; DATABASE SYSTEMS; LOADS (FORCES); PARAMETER ESTIMATION; TRAJECTORIES; WIND TUNNELS;

DATABASE GENERATION; NOISE PARAMETERS; TEST DATA; TRAJECTORY ANALYSIS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 20744460601 PISSN: 10485953 EISSN: None Source Type: Conference Proceeding
DOI: 10.2514/6.2004-4724 Document Type: Conference Paper

Times cited : (9)

References (11)

1
- 20744444055
- AIAA 94-3454
- Sickles, et al., "Separation of the Pegasus XL from an L-1011 Aircraft", AIAA 94-3454
- Separation of the Pegasus XL from An L-1011 Aircraft
- Sickles¹

2
- 84896693039
- Beggar - A store separation predictive tool
- AIAA Paper 02-3190, St. Louis, Missouri, June
- Rizk, Magdi, Ellison, Steven and Prewitt, Nathan C., "Beggar - A Store Separation Predictive Tool"; AIAA Paper 02-3190, 32 Fluid Dynamics Conference and Exhibit, St. Louis, Missouri, June 2002
- (2002) 32 Fluid Dynamics Conference and Exhibit
- Rizk, M.¹ Ellison, S.² Prewitt, N.C.³

3
- 2942717026
- Beggar code Implementation of (6+)-DOF capability for stores with moving components
- Reno, Nevada, Jan 5-8
- nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, Jan 5-8, 2004
- (2004) nd AIAA Aerospace Sciences Meeting and Exhibit
- Rizk, M.¹ Lee, J.M.²

4
- 78649843665
- Inviscid store separation during transonic flight with deployable fins using (6+) DOF
- San Diego La Jolla, California, July 25-29
- th International Bi-Annual ASME/JSME Symposium, San Diego La Jolla, California, July 25-29, 2004
- (2004) th International Bi-annual ASME/JSME Symposium
- Dudley, J.G.¹ Westmoreland, W.S.²

5
- 85067320349
- A comparison of inviscid and viscous approaches for store separations
- AIAA Paper 021413, St. Louis, Missouri, June
- th Applied Aerodynamics Conference, St. Louis, Missouri, June 2002
- (2002) th Applied Aerodynamics Conference
- Westmoreland, S.¹

6
- 0004238551
- Macmillan Publishing Company, New York
- Hogg, Robert V., Tanis, Elliot A., "Probability and Statistical Interference", Macmillan Publishing Company, New York
- Probability and Statistical Interference
- Hogg, R.V.¹ Tanis, E.A.²

7
- 0003722376
- Addison-Wesley
- Goldberg, David E., "Genetic Algorithms in Search and Machine Learning" 1989. Addison-Wesley.
- (1989) Genetic Algorithms in Search and Machine Learning
- Goldberg, D.E.¹

8
- 0004186280
- Dover Publications, Inc., New York
- Bisplinghoff, Raymond L., Ashley, Holt, "Principles of Aeroelasticity", Dover Publications, Inc., New York
- Principles of Aeroelasticity
- Bisplinghoff, R.L.¹ Ashley, H.²

9
- 20744436614
- School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia
- Pierce, G. Alvin, "Potential Flow - Class Note"; School of Aerospace Engineering, Georgia Institute of Technology, Atlanta, Georgia
- Potential Flow - Class Note
- Pierce, G.A.¹

10
- 85067321534
- CFD investigation of Plastic Practice Bomb (PPB) separation from F16/TER-9A configuration
- American Institute of Aeronautics and Astronautics, Orlando, FL, June 23-26
- st Applied Aerodynamics Conference, American Institute of Aeronautics and Astronautics, Orlando, FL, June 23-26, 2003
- (2003) st Applied Aerodynamics Conference
- Lee, J.M.¹ Dunworth, K.² Chesser, B.L.³ Ellison, S.⁴ Jolly, B.⁵

11
- 20744445470
- Use of CFD-generated aerodynamic data for an F-15E/SLV flying/handling qualities analysis
- September
- Westmoreland, S., Batte, J., "Use of CFD-Generated Aerodynamic Data for an F-15E/SLV Flying/Handling Qualities Analysis", Stability and Control Conference, September 2003
- (2003) Stability and Control Conference
- Westmoreland, S.¹ Batte, J.²

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