-
4
-
-
0004807561
-
-
Rockwell International Space Division, Rept. SD 72-SH-0060-1L, Downey, CA, Nov.
-
Aerodynamic Design Data Book, Vol. I, Orbiter Vehicle, Rockwell International Space Division, Rept. SD 72-SH-0060-1L, Downey, CA, Nov. 1977.
-
(1977)
Aerodynamic Design Data Book, Vol. I, Orbiter Vehicle
, vol.1
-
-
-
5
-
-
0035332144
-
Aerodynamic characteristics, database development, and flight simulation of the X-34 vehicle
-
Pamadi, B.N. Brauckmann, G.J., Ruth, M.J., and Fuhrmann, H.D., Aerodynamic Characteristics, Database Development, and Flight Simulation of the X-34 Vehicle, Journal of Spacecraft and Rockets, Vol. 38, No. 3, pp 334-344.
-
Journal of Spacecraft and Rockets
, vol.38
, Issue.3
, pp. 334-344
-
-
Pamadi, B.N.1
Brauckmann, G.J.2
Ruth, M.J.3
Fuhrmann, H.D.4
-
6
-
-
22544456146
-
The NASA langley 16- foot transonic tunnel
-
Sept.
-
Capone, F.J., Bangert, L.S., Asbury, S.C., Mills, C.T., and Bare, E.A.: The NASA Langley 16- Foot Transonic Tunnel, NASA TP-3521, Sept. 1995.
-
(1995)
NASA TP-3521
-
-
Capone, F.J.1
Bangert, L.S.2
Asbury, S.C.3
Mills, C.T.4
Bare, E.A.5
-
7
-
-
85040284939
-
Description and calibration of the langley unitary plan wind tunnel
-
Nov.
-
Jackson, C.M., Corlett, W.A., and Monta, W.J.: Description and Calibration of the Langley Unitary Plan Wind Tunnel, NASA TP-1905, Nov. 1981.
-
(1981)
NASA TP-1905
-
-
Jackson, C.M.1
Corlett, W.A.2
Monta, W.J.3
-
8
-
-
85067322174
-
Stage separation wind tunnel tests of a generic two-stage-to-orbit launch vehicle
-
July
-
Borderlon, W. J., Frost, A.L., and Reed, D, K.: Stage Separation Wind Tunnel Tests of a Generic Two-Stage-to-Orbit Launch Vehicle, AIAA Paper 2003-4227, July 2003.
-
(2003)
AIAA Paper
, vol.2003
, Issue.4227
-
-
Borderlon, W.J.1
Frost, A.L.2
Reed, D.K.3
-
9
-
-
20544433511
-
Use of grit-type boundary-layer-transition trips on wind-tunnel models
-
Braslow, Albert I.; Hicks, Raymond M.; and Harris, Roy V., Jr.: Use of Grit-Type Boundary-Layer-Transition Trips on Wind-Tunnel Models. NASA TN D-3579, 1966.
-
(1966)
NASA TN D-3579
-
-
Braslow, A.I.1
Hicks, R.M.2
Harris Jr., R.V.3
-
10
-
-
20544446520
-
Effects of roughness size on the position of boundary-layer-transition and on the aerodynamic characteristics of a 55-degree swept delta wing at supersonic speeds
-
Stallings, Robert L., Jr.; and Lamb, Milton: Effects of Roughness size on the Position of Boundary-Layer-Transition and on the Aerodynamic Characteristics of a 55-degree Swept Delta Wing at Supersonic Speeds. NASA TP-1027, 1977.
-
(1977)
NASA TP-1027
-
-
Stallings Jr., R.L.1
Lamb, M.2
-
11
-
-
20544439707
-
Procedures and requirements for testing in the langley research center unitary plan wind tunnel
-
Wassum, Donald L.; and Hyman, Curtis E., Jr.: Procedures and Requirements for Testing in the Langley Research Center Unitary Plan Wind Tunnel. MASA TM-100529, 1988.
-
(1988)
MASA TM-100529
-
-
Wassum, D.L.1
Hyman Jr., C.E.2
-
12
-
-
0004757440
-
Aerodynamic preliminary analysis system ii, part i- theory
-
April
-
Bonner, E., Clever, W., and Dunn, K.: Aerodynamic Preliminary Analysis System II, Part I- Theory, NASA CR-182076, April 1991.
-
(1991)
NASA CR-182076
-
-
Bonner, E.1
Clever, W.2
Dunn, K.3
-
13
-
-
0342601822
-
Aerodynamic preliminary analysis system ii, part ii- user's manual
-
April
-
Sova, G. and Divan P.: Aerodynamic Preliminary Analysis System II, Part II- User's Manual, NASA CR-182077, April 1991.
-
(1991)
NASA CR-182077
-
-
Sova, G.1
Divan, P.2
-
14
-
-
18844404782
-
Capabilities and application of the program to optimize simulated trajectories
-
February
-
Brauer, G.I., Cornick, D.E., and Stevenson, R., Capabilities and Application of the Program to Optimize Simulated Trajectories, NASA CR-2770, February 1977.
-
(1977)
NASA CR-2770
-
-
Brauer, G.I.1
Cornick, D.E.2
Stevenson, R.3
-
15
-
-
20544454938
-
The NASA/ MSFC global reference atmospheric model - 1999 Version (GRAM-99)
-
May
-
Justus, C.G. and Johnson, D.L., "The NASA/ MSFC Global Reference Atmospheric Model - 1999 Version (GRAM-99)," NASA TM-1999-209630, May 1999.
-
(1999)
NASA TM-1999-209630
-
-
Justus, C.G.1
Johnson, D.L.2
-
16
-
-
2942754058
-
Ascent, stage separation and glideback performance of a partially reusable small launch vehicle
-
Pamadi, B.N., Tartabini, P.V., and Starr, B.R., Ascent, Stage Separation and Glideback Performance of a Partially Reusable Small Launch Vehicle, AIAA Paper 2004-0876.
-
AIAA Paper
, vol.2004
, Issue.876
-
-
Pamadi, B.N.1
Tartabini, P.V.2
Starr, B.R.3
-
17
-
-
1842721928
-
Robust and efficient cartesian mesh generation for component-based geometry
-
Jan.
-
Aftosmis M.J., Berger M.J., and Melton J.E., "Robust and Efficient Cartesian Mesh Generation for Component-Based Geometry", AIAA Paper 97-0196. Jan. 1997.
-
(1997)
AIAA Paper
, vol.97
, Issue.196
-
-
Aftosmis, M.J.1
Berger, M.J.2
Melton, J.E.3
-
18
-
-
84982318348
-
Recent enhancements to OVERFLOW
-
Jan.
-
Jespersen D.C., Pulliam T.H., and Buning P.G., "Recent Enhancements to OVERFLOW", AIAA Paper 97-0644, Jan. 1997.
-
(1997)
AIAA Paper
, vol.97
, Issue.644
-
-
Jespersen, D.C.1
Pulliam, T.H.2
Buning, P.G.3
|