Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model /

MAVRIC flutter model transonic limit cycle oscillation test /
by: Edwards, John W.
Published: (2001)

A historical overview of Aeroelasticity Branch and Transonic Dynamics Tunnel contributions to rotorcraft technology and development /
by: Yeager, William T.
Published: (2001)

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

Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle /
by: Lamb, Milton
Published: (1985)

Estimated benefits of variable-geometry wing camber control for transport aircraft /
by: Bolonkin, Alexander, et al.
Published: (1999)

Computational analysis of a low-boom supersonic inlet /
by: Chima, Rodrick V.
Published: (2011)

Experimental and theoretical study of the longitudinal aerodynamic characteristics of delta and double-delta wings at mach numbers of 1.60, 1.90, and 2.16 /
by: Wood, Richard M., et al.
Published: (1985)

Experimental effects of wing location on wing-body pressures at supersonic speeds /
by: Allen, Jerry M., et al.
Published: (1993)

Supersonic through-flow fan engine and aircrraft mission performance /
by: Franciscus, Leo C.
Published: (1989)

Nacelle-pylon-wing integration on a transport model with a natural laminar flow nacelle /
by: Lamb, Milton
Published: (1985)

Loop Shaping control design for a supersonic propulsion system model using quantitative feedback theory (QFT) specifications and bounds /
by: Connolly, Joseph W.
Published: (2010)

Supersonic wind tunnel nozzles : a selected, annotated bibliography to aid in the development of quiet wind tunnel technology /
by: Wolf, Stephen W. D.
Published: (1990)

Two-dimensional aerodynamic characteristics of the OLS/TAAT airfoil /
by: Watts, Michael E., et al.
Published: (1988)

NASA Ames Laminar Flow Supersonic Wind Tunnel (LFSWT) tests of a 10 ̊cone at Mach 1.6 /
by: Wolf, Stephen W. D., et al.
Published: (1997)

Study of high-speed civil transports /
Published: (1989)

Experimental and theoretical study of longitudinal aerodynamic characteristics of delta and double-delta wings at Mach numbers of 1.60, 1.90, and 2.16 /
by: Wood, Richard M., et al.
Published: (1985)

Enabling rapid and robust structural analysis during conceptual design /
by: Eldred, Lloyd B., et al.
Published: (2015)

Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover /
by: Watkins, Anthony Neal
Published: (2018)

Assessment of NASA's aircraft noise prediction capability /
Published: (2012)

Evaluation of low noise integration concepts and propulsion technologies for future supersonic civil transports /
by: Ramakrishnan, Kishore
Published: (2018)

Integration effects of D-shaped, underwing, aft-mounted, separate-flow, flow-through nacelles on a high-wing transport /
by: Lamb, Milton, et al.
Published: (1987)

Final report for the advanced concept studies for supersonic commercial transports entering service in the 2030 to 2035 period, N+3 Supersonic Program /
Published: (2010)

Hot-bench simulation of the active flexible wing wind-tunnel model /
by: Buttrill, Carey S.
Published: (1990)

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)

Nozzle plume/shock interaction experimental and computational sonic boom analyses from the NASA Ames 9-by 7-foot supersonic wind tunnel /
by: Durston, D. A.
Published: (2018)

Measurements of fluctuating pressures in 8- by 6-foot supersonic wind tunnel for Mach number range of 0.56 to 2.07 /
by: Karabinus, Raymond J., et al.
Published: (1970)

Flow quality survey of the 8-by 6-foot supersonic wind tunnel (2015 test) prior to the 9-by 15-foot low-speed wind tunnel acoustic improvement modifications /
by: Johnson, Aaron M.
Published: (2018)

An aerodynamic tradeoff study of the scissor wing configuration /
by: Selberg, Bruce P.
Published: (1990)

Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations /
by: Hess, R. W. (Robert W.), et al.
Published: (1986)

Supersonic cruise technology /
by: McLean, F. Edward
Published: (1985)

Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ /
by: Spearman, M. Leroy
Published: (1985)

An experimental device for generating high frequency perturbations in supersonic wind tunnels /
by: Melcher, Kevin J., et al.
Published: (1996)

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)

Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena /
by: Kegerise, Michael A., et al.
Published: (2016)

Feasibility and benefits of laminar flow control on supersonic cruise airplanes /
by: Powell, A. G.
Published: (1989)

Feasibility and benefits of laminar flow control on supersonic cruise airplanes /
by: Powell, A. G.
Published: (1989)