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Journal of Propulsion and Power

Volumn 17, Issue 2, 2001, Pages 276-283

Experimental testing of a hypersonic inlet with rectangular-to-elliptical shape transition

(1) Smart, M K a

a NASA LANGLEY RESEARCH CENTER (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRFRAMES; HYPERSONIC FLOW; INTAKE SYSTEMS; MATHEMATICAL MODELS; SUPERSONIC FLOW;

HYPERSONIC INLETS; MACH NUMBER;

WIND TUNNELS;

EID: 0035280057 PISSN: 07484658 EISSN: 15333876 Source Type: Journal
DOI: 10.2514/2.5774 Document Type: Article

Times cited : (128)

References (12)

1
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- U.S. Air Force Rept. AFAPL-TR-65-74, Marquardt Corp., Aug.
- (1965) Analytical and Experimental Investigation of a Scramjet Inlet of Quadriform Shape
- Hartill, W.B.¹

2
- 0029407557
- Supersonic combustion ramjet missile
- (1995) Journal of Propulsion and Power , vol.11 , Issue.6 , pp. 1139-1146
- Billig, F.S.¹

3
- 0005453788
- General Electric Co. Advanced Engine and Technology Departments, Cincinnati, OH, June
- (1965) Hypersonic Inlet Tests in Helium and Air
- Kutshenreuter, P.H.¹

4
- 0003841979
- CP-30, AGARD
- (1968) Modular Hypersonic Inlets with Conical Flow
- Molder, S.¹ Romeskie, J.M.²

5
- 0005509904
- NACA WR L-713
- (1945) Preliminary Investigation of Supersonic Diffusers
- Kantrowitz, A.¹ Donaldson, C.²

6
- 0033131888
- Design of three-dimensional hypersonic inlets with rectangular-to-elliptical shape transition
- (1999) Journal of Propulsion and Power , vol.15 , Issue.3 , pp. 408-416
- Smart, M.K.¹

7
- 0005453789
- AIAA Paper 96-3243, July
- (1996) The NASA Langley Scramjet Test Complex
- Guy, R.W.¹ Rogers, R.C.² Puster, R.L.³ Rock, K.E.⁴ Diskin, G.S.⁵

8
- 84997235778
- AIAA Paper 87-2165, June
- (1987) Test Flow Calibration Study of the Langley Arc- Heated Scramjet Test Facility
- Thomas, S.R.¹ Voland, R.T.² Guy, R.W.³

9
- 0016048610
- Improved static probe design
- (1974) AIAA Journal , vol.12 , Issue.4 , pp. 562
- Pinckney, S.Z.¹

10
- 0005416360
- NASA TP-3447, Sept.
- (1994) Computer Code for Determination of Thermally Perfect Gas Properties
- Witte, D.W.¹ Tatum, K.E.²

11
- 85037424333
- A comparison of three hypersonic inlets
- Sec. 6 , U.S. Air Force Rept. WL-TR-93-2091, Ryerson Polytechnic Inst., Toronto
- (1993) Investigations in the Fluid Mechanics of Scramjet Inlets
- Molder, S.¹ McGregor, R.J.² Paisley, T.W.³

12
- 0005417237
- AIAA Paper 96-2914, July
- (1996) Starting Characteristics of Supersonic Inlets
- Van Wie, D.M.¹ Kwok, F.T.² Walsh, R.F.³

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.