SCOPUS 정보 검색 플랫폼

U.S. Air Force T and E Days

Volumn , Issue , 2008, Pages

Swept-wing laminar flow control studies using Cessna O-2A test aircraft

(3) Martin, Marvin L a Carpenter, Andrew L b Saric, William S b

a NORTHROP GRUMMAN CORPORATION (United States)

b TEXAS A AND M UNIVERSITY (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ANGLE OF ATTACK; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYERS; CIVIL AVIATION; IMAGING TECHNIQUES; LAMINAR FLOW; REYNOLDS NUMBER; TESTING; TURBULENCE;

BOUNDARY LAYER STABILITIES; FREESTREAM TURBULENCE; IN-DYNAMIC STABILITIES; LAMINAR TO TURBULENT TRANSITIONS; NATURAL LAMINAR FLOWS; QUALITATIVE IMAGING; ROUGHNESS ELEMENTS; TURBULENCE INTENSITY;

SWEPT WINGS;

EID: 77958167960 PISSN: None EISSN: None Source Type: Conference Proceeding
DOI: 10.2514/6.2008-1636 Document Type: Conference Paper

Times cited : (11)

References (9)

1
- 51349101201
- TAMUS-AE-TR-06-001, Technical Report, January 2006
- Saric WS, Carpenter AL, Hunt LE, Kluzek CD 2006a. "SWIFT - Flight Test Plan for Swept-Wing Experiments." TAMUS-AE-TR-06-001, Technical Report, January 2006
- (2006) SWIFT - Flight Test Plan for Swept-Wing Experiments
- Saric, W.S.¹ Carpenter, A.L.² Hunt, L.E.³ Kluzek, C.D.⁴

2
- 77958165565
- TAMUS-AE-TR-06-003, Technical Report, January 2006
- Saric WS, Carpenter AL, Hunt LE, Kluzek CD 2006c. "Cessna O-2 General Flight Test Procedures: Operations for the Flight Research Laboratory." TAMUS-AE-TR-06-003, Technical Report, January 2006
- (2006) Cessna O-2 General Flight Test Procedures: Operations for the Flight Research Laboratory
- Saric, W.S.¹ Carpenter, A.L.² Hunt, L.E.³ Kluzek, C.D.⁴

3
- 51349150741
- TAMUS-AE-TR-06-002, Technical Report, January 2006
- Saric WS, Carpenter AL, Hunt LE, McKnight CW, Schouten SM 2006b. "SWIFT - Safety Analysis for Swept-Wing Experiments." TAMUS-AE-TR-06-002, Technical Report, January 2006
- (2006) SWIFT - Safety Analysis for Swept-Wing Experiments
- Saric, W.S.¹ Carpenter, A.L.² Hunt, L.E.³ McKnight, C.W.⁴ Schouten, S.M.⁵

4
- 77958167229
- Vibration and flutter analysis
- Schultz W. H., Pate C, Geide R, Ahrens DJ, Gerteis JH 1967. Vibration and Flutter Analysis. Cessna Report No. S-M337-27-3
- (1967) Cessna Report No. S-M337-27-3
- Schultz, W.H.¹ Pate, C.² Geide, R.³ Ahrens, D.J.⁴ Gerteis, J.H.⁵

5
- 77958163924
- Master's Thesis, ETD-TAMU-2006B-AERO-McKnight
- McKnight, CW 2006. Design and Safety Analysis of an In-Flight, Test Airfoil. Master's Thesis, ETD-TAMU-2006B-AERO-McKnight.
- (2006) Design and Safety Analysis of An In-Flight, Test Airfoil
- McKnight, C.W.¹

6
- 51349165334
- Infrared thermography investigations in transitional supersonic boundary layers
- in press
- Zuccher S, Saric WS 2006. Infrared Thermography Investigations in Transitional Supersonic Boundary Layers. Exps. Fluids, in press.
- (2006) Exps. Fluids
- Zuccher, S.¹ Saric, W.S.²

7
- 77958164401
- RTO-MP-AVT-111/RSM
- Saric WS, Reed HL, Banks DW 2005. Flight Testing of Laminar Flow Control in High-Speed Boundary Layers. RTO-MP-AVT-111/RSM.
- (2005) Flight Testing of Laminar Flow Control in High-Speed Boundary Layers
- Saric, W.S.¹ Reed, H.L.² Banks, D.W.³

8
- 0033225650
- Effect of isolated micron-sized roughness on transition in swept-wing flows
- Radeztsky, RH, Reibert, M, Saric, WS 1999. Effect of Isolated Micron-Sized Roughness on Transition in Swept-Wing Flows. AIAA J., Vol. 37, No. 11, pp. 1370-77
- (1999) AIAA J. , vol.37 , Issue.11 , pp. 1370-1377
- Radeztsky, R.H.¹ Reibert, M.² Saric, W.S.³

9
- 84982318118
- Leading-edge roughness as a transition control mechanism
- Saric WS, Carrillo R, Reibert M 1998a. Leading-edge Roughness as a Transition Control Mechanism. AIAA Paper No. 98-0781
- (1998) AIAA Paper No. 98-0781
- Saric, W.S.¹ Carrillo, R.² Reibert, M.³

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.