Space shuttle orbiter trimmed center-of-gravity extension study. Volume ix, Effects of configuration modifications on the aerodynamic characteristics of the 140 A/B orbiter at mach numbers of 1.5, 2.0, and 2.5 /

Determination of shuttle orbiter center of gravity from flight measurements /
by: Hinson, E. W.
Published: (1991)

Space shuttle phase B wind tunnel model and test information.
by: Glynn, J. L.
Published: (1988)

Pressure distributions on a 0.02-scale space shuttle orbiter nose at Mach 21.5 in helium /
by: Ashby, George C., et al.
Published: (1994)

Experimental aerodynamic heating to simulated shuttle tiles /
by: Avery, Don E., et al.
Published: (1983)

Dynamic assessment of B-52B-008 carrier aircraft for the revised space shuttle solid rocket booster decelerator subsystem drop test vehicle.
by: Doty, Leslie J.
Published: (1983)

Effect of canard position and wing leading-edge flap deflection on wing buffet at transonic speeds /
by: Gloss, Blair B., et al.
Published: (1975)

Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /
by: Mack, Robert J.
Published: (1999)

Cavity heating experiments supporting Shuttle Columbia accident investigation /
Published: (2011)

Inviscid flow computations of the shuttle orbiter for Mach 10 and 15 and angle of attack 40 to 60 degrees /
by: Prabhu, Ramadas K.
Published: (2001)

Study of several factors affecting crew escape trajectories from the space shuttle orbiter at low-subsonic speeds /
Published: (1985)

Space shuttle afterbody aerodynamics/plume simulation data summary /
by: Blackwell, Kenneth L., et al.
Published: (1978)

Independent Orbiter assessment : assessment of the manned maneuvering unit /
by: Huynh, M.
Published: (1988)

Use of hyperbolic grid generation scheme in simulating supersonic viscous flow about three-dimensional winged configurations /
by: Rizk, Yehia M., et al.
Published: (1985)

Aero-heating of shallow cavities in hypersonic freestream flow /
Published: (2010)

Flow-visualization techniques used at high speed by configuration aerodynamics wind-tunnel-test team /
Published: (2001)

Hybrid wing body shielding studies using an ultrasonic configurable fan artificial noise source generating typical turbofan modes /
by: Sutliff, Daniel L. (Daniel Linden), 1962-, et al.
Published: (2014)

Prediction of forces and moments for flight vehicle control effectors /
Published: (1990)

Feasibility analysis of cislunar flight using the shuttle orbiter /
by: Haynes, Davy A.
Published: (1991)

The Langley 14- by 22-foot subsonic tunnel : description, flow characteristics, and guide for users /
Published: (1990)

Parametric study of a canard-configured trasport using conceptual design optimization /
by: Arbuckle, P. Douglas, et al.
Published: (1985)

Wind tunnel investigation of passive vortex control and vortex-tail interactions on a slender wing at subsonic and transonic speeds /
by: Erickson, Gary E.
Published: (2013)

Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses /
by: Harris, Charles D., 1952-
Published: (1972)

Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles /
by: Castner, Raymond S.
Published: (2010)

Study of the integration of wind tunnel and computational methods for aerodynamic configurations /
by: Browne, Lindsay E.
Published: (1989)

Aeroelastic sizing for high-speed research (HSR) longitudinal control alternatives project (LCAP) /
Published: (2005)

Space Shuttle flying qualities criteria assessment--phase III /
by: Myers, T. T., et al.
Published: (1984)

Static wind-tunnel and radio-controlled flight test investigation of a remotely piloted vehicle having a delta wing planform /
Published: (1990)

Extraction of stability and control derivatives from orbiter flight data /
by: Iliff, Kenneth W., et al.
Published: (1993)

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /
by: Schuster, D. M. (David M.)
Published: (2001)

Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel /
by: Schuster, D. M. (David M.)
Published: (2001)

Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration /
by: Campbell, Bryan A.
Published: (1999)

Modeling and control study of the NASA 0.3-meter transonic cryogenic tunnel for use with sulfur hexafluoride medium /
by: Balakrishna, S.
Published: (1992)

Unsteady velocity measurements taken behind a model helicopter rotor hub in forward flight /
by: Berry, John D.
Published: (1997)

Exploratory low-speed wind-tunnel study of concepts designed to improve aircraft stability and control at high angles of attack /
by: Hahne, David E. (David Edgar)
Published: (1985)

Effect of protuberance shape and orientation on Space Shuttle Orbiter boundary-layer transition /
by: King, Rudolph A.
Published: (2008)

Prediction of vortex-induced loads on wind tunnel turning vanes /
by: Ross, James C., 1965-
Published: (1985)