SCOPUS 정보 검색 플랫폼

21st Aerodynamic Measurement Technology and Ground Testing Conference

Volumn , Issue , 2000, Pages

Test capabilities and recent experiences in the NASA Langley 8-foot high temperature tunnel

(2) Hodge, Jeffrey S a Harvin, Stephen F a

a NASA LANGLEY RESEARCH CENTER (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; FLIGHT SIMULATORS; NASA; OXYGEN; PROPULSION;

AIR BREATHING PROPULSIONS; AIR-BREATHING PROPULSION; COMBUSTION PRODUCTS; GENERAL DESCRIPTION; HYPERSONIC PROPULSION SYSTEMS; OPEN-JET TEST SECTIONS; PRESSURIZED COMBUSTION; THERMAL PROTECTION SYSTEM;

WIND TUNNELS;

EID: 84995771783 PISSN: None EISSN: None Source Type: Conference Proceeding
DOI: 10.2514/6.2000-2646 Document Type: Conference Paper

Times cited : (15)

References (7)

1
- 84894345048
- NASA TM X-2767, May
- Wieting, A. R.: "Aerodynamic and Thermal Analysis of Results of Tests of a Hydrogen Cooled Scramjet Engine at Mach 6. 3, " NASA TM X-2767, May 1973.
- (1973) Aerodynamic and Thermal Analysis of Results of Tests of a Hydrogen Cooled Scramjet Engine At Mach 6. 3
- Wieting, A.R.¹

2
- 84894550867
- NASA TN D-8150, March
- Hunt, L. R.; Shideler, J. L.; and Weinstein, I.: Performance of LI-1542 Reusable Surface Insulation in a Hypersonic Stream/' NASA TN D-8150, March 1976,
- (1976) Performance of LI-1542 Reusable Surface Insulation In a Hypersonic Stream
- Hunt, L.R.¹ Shideler, J.L.² Weinstein, I.³

3
- 84997132388
- AIAA Paper 87-1887, June
- Reubush, D. E.; Puster, R. L.; and Kelly, H. N.: "Modification to the Langley 8-Foot High Temperature Tunnel for Hypersonic Propulsion Testing, " AIAA Paper 87-1887, June 1987.
- (1987) Modification to The Langley 8-Foot High Temperature Tunnel For Hypersonic Propulsion Testing
- Reubush, D.E.¹ Puster, R.L.² Kelly, H.N.³

4
- 84983121010
- AIAA Paper 96-2197, June
- Huebner, L. D.; Rock, K. E.; Voland, R. T.; and Wieting, A. R.: "Calibration of the Langley 8-Foot High Temperature Tunnel for Hypersonic Airbreathing Propulsion Testing, " AIAA Paper 96-2197, June 1996.
- (1996) Calibration of the Langley 8-Foot High Temperature Tunnel For Hypersonic Airbreathing Propulsion Testing
- Huebner, L.D.¹ Rock, K.E.² Voland, R.T.³ Wieting, A.R.⁴

5
- 84894548089
- NASP Report X30SP94007, January, SECRET
- Phelps, D. C.; McVey, W. J.; and Faulkner, R. F.: "National Aerospace Plane Concept Demonstration Engine Final Test Report (U). NASP Report X30SP94007, January 1995. (SECRET)
- (1995) National Aerospace Plane Concept Demonstration Engine Final Test Report (U)
- Phelps, D.C.¹ McVey, W.J.² Faulkner, R.F.³

6
- 84894570399
- To be presented at the 1999 JANNAF CS/PSHS/APS Joint Meetings, Cocoa Beach, FL, October 18-22
- Witte, D. W.; Ruf E. G.; Fischer, K. E.; Huebner, L. D.; and Andrews, E. H.: Results of the Mach 7 Hyper-X Engine Model Test in the NASA Langley 8-Foot High Temperature Tunnel (U). To be presented at the 1999 JANNAF CS/PSHS/APS Joint Meetings, Cocoa Beach, FL, October 18-22, 1999.
- (1999) Results of the Mach 7 Hyper-X Engine Model Test In the NASA Langley 8-Foot High Temperature Tunnel (U)
- Witte, D.W.¹ Ruf, E.G.² Fischer, K.E.³ Huebner, L.D.⁴ Andrews, E.H.⁵

7
- 0004023831
- To be presented at the 1999 JANNAF CS/PSHS/APS Joint Meetings, Cocoa Beach, FL, October 18-00 1000
- Huebner L. D.; Rock, K. E.; Witte, D. W.; Curro, J. M.; and Andrews, E. H.: "Overview of Hyper-X Engine Tests in the NASA Langley 8-Foot High Temperature Tunnel. " To be presented at the 1999 JANNAF CS/PSHS/APS Joint Meetings, Cocoa Beach, FL, October 18-00 1000
- Overview of Hyper-X Engine Tests In the NASA Langley 8-Foot High Temperature Tunnel
- Huebner, L.D.¹ Rock, K.E.² Witte, D.W.³ Curro, J.M.⁴ Andrews, E.H.⁵

* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.