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Experiments in Fluids

Volumn 22, Issue 3, 1997, Pages 183-190

Transition on a slender cone in hypervelocity flow

(2) Germain, P D a Hornung, H G a

a CALIFORNIA INSTITUTE OF TECHNOLOGY (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0000655801 PISSN: 07234864 EISSN: None Source Type: Journal
DOI: 10.1007/s003480050036 Document Type: Article

Times cited : (68)

References (13)

1
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- Demetriades, A.¹

2
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- Report AFOSR-TR-77-1311, Air Force Office of Scientific Research, Washington, DC
- Demetriades A (1977) Laminar boundary layer stability measurements at Mach 7 including wall temperature effects. Report AFOSR-TR-77-1311, Air Force Office of Scientific Research, Washington, DC
- (1977) Laminar Boundary Layer Stability Measurements at Mach 7 Including Wall Temperature Effects
- Demetriades, A.¹

3
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- Three-dimensional laminar boundary-layer transition on a sharp 8° cone at Mach 10
- DiCristina V (1970) Three-dimensional laminar boundary-layer transition on a sharp 8° cone at Mach 10. AIAA J 8: 852-856
- (1970) AIAA J , vol.8 , pp. 852-856
- DiCristina, V.¹

4
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- Transition of compressible high enthalpy boundary layer over a flat plate
- He Y; Morgan RG (1994) Transition of compressible high enthalpy boundary layer over a flat plate. Aeronaut J 98: 25-34
- (1994) Aeronaut J , vol.98 , pp. 25-34
- He, Y.¹ Morgan, R.G.²

5
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- AIAA Paper no. 92-3943
- Hornung HG (1992) Performance data of the new free-piston shock tunnel at GALCIT. AIAA Paper no. 92-3943
- (1992) Performance Data of the New Free-piston Shock Tunnel at GALCIT
- Hornung, H.G.¹

6
- 0016483071
- Wind tunnel experiments relating to supersonic and hypersonic boundary-layer transition
- Kendall JM (1975) Wind tunnel experiments relating to supersonic and hypersonic boundary-layer transition. AIAA J 13: 290-299
- (1975) AIAA J , vol.13 , pp. 290-299
- Kendall, J.M.¹

7
- 85003234554
- Report 900-277 Rev A, Jet Propulsion Laboratory, Pasadena, California
- Mack LM (1969) Boundary layer stability. Report 900-277 Rev A, Jet Propulsion Laboratory, Pasadena, California
- (1969) Boundary Layer Stability
- Mack, L.M.¹

8
- 0010052819
- Real gas effects on hypersonic boundary layer stability
- Malik MR; Anderson EC (1991) Real gas effects on hypersonic boundary layer stability. Phys Fluids A 3: 803-821
- (1991) Phys Fluids A , vol.3 , pp. 803-821
- Malik, M.R.¹ Anderson, E.C.²

9
- 0016483141
- Comparison of wind tunnel transition and freestream disteurbance measurements
- Owen FK; Horstman CC; Stainback PC (1975) Comparison of wind tunnel transition and freestream disteurbance measurements. AIAA J 13: 266-269
- (1975) AIAA J , vol.13 , pp. 266-269
- Owen, F.K.¹ Horstman, C.C.² Stainback, P.C.³

10
- 0016482883
- Boundary-layer transition on supersonic cones in an aeroballistic range
- Potter JL (1975) Boundary-layer transition on supersonic cones in an aeroballistic range. AIAA J 13: 270-277
- (1975) AIAA J , vol.13 , pp. 270-277
- Potter, J.L.¹

11
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- AIAA Paper no. 94-0001
- Reshotko E (1994) Boundary layer instability, transition and control. AIAA Paper no. 94-0001
- (1994) Boundary Layer Instability, Transition and Control
- Reshotko, E.¹

12
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- Stetson, K.F.¹

13
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- AIAA Paper no. 90-1529
- Stuckert GK; Reed HL (1990) Stability of hypersonic, chemically reacting viscous flows. AIAA Paper no. 90-1529
- (1990) Stability of Hypersonic, Chemically Reacting Viscous Flows
- Stuckert, G.K.¹ Reed, H.L.²

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.