Jump to main content

yr 〜
yr

Search results 6

Hyper-X Engine testing in the NASA Langley 8-Foot High Temperature Tunnel AIAA-2000-3605

Hyper-X Engine testing in the NASA Langley 8-Foot High Temperature Tunnel AIAA-2000-3605
Paper規格・テクニカルリポート類
Huebner, Lawrence D, Rock, Kenneth E, Witte, David W, Ruf, Edward G, Andrews, Earl H., Jr2000<M-AIAA-2000-3605>
National Diet Library

Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations [microform] / Charles E. Cockrell, Jr. and Lawrence D. Huebner, Dennis B. Finley (NASA technical paper ; 3559)

Aerodynamic characteristics of two waverider-derived hypersonic cruise configurations [microform] / Charles E. Cockrell, Jr. and Lawrence D. Huebner, Dennis B. Finley (NASA technical paper ; 3559)
Microform図書
1996<YCA-NAS 1.60:3559>
National Diet Library
  • Author HeadingCockrell, Charles E Huebner, Lawrence D Finley, Dennis B Langley Rese...

Exhaust gas modeling effects on hypersonic powered simulation at Mach 10 AIAA-95-6068

Exhaust gas modeling effects on hypersonic powered simulation at Mach 10 AIAA-95-6068
Paper規格・テクニカルリポート類
Tatum, Kenneth E, Huebner, Lawrence D1995<M-AIAA-95-6068>
National Diet Library

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation [microform] / Lawrence D. Huebner, Marc W. Kniskern, William J. Monta (NASA technical memorandum ; 4441)

Assessment of a flow-through balance for hypersonic wind tunnel models with scramjet exhaust flow simulation [microform] / Lawrence D. Huebner, Marc W. Kniskern, William J. Monta (NASA technical memorandum ; 4441)
Microform図書
1993<YCA-NAS 1.15:4441>
National Diet Library
  • Author HeadingHuebner, Lawrence D Kniskern, Marc W Monta, Willi...

Experimental results on the feasibility of an aerospike for hypersonic missiles AIAA-95-0737

Experimental results on the feasibility of an aerospike for hypersonic missiles AIAA-95-0737
Paper規格・テクニカルリポート類
Huebner, Lawrence D, Mitchell, Anthony M, Boudreaux, Ellis J<M-AIAA-95-0737>
National Diet Library

Aerodynamic performance and flow-field characteristics of two waverider-derived hypersonic cruise configurations AIAA-95-0736

Aerodynamic performance and flow-field characteristics of two waverider-derived hypersonic cruise configurations AIAA-95-0736
Paper規格・テクニカルリポート類
Cockrell, Charles E., Jr, Huebner, Lawrence D, Finley, Dennis B<M-AIAA-95-0736>
National Diet Library

Reached to the end of result.

RSS