Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds /

Supersonic inlet test for a quiet supersonic transport technology demonstrator in the NASA Glenn 8-by 6-foot supersonic wind tunnel /
by: Castner, Raymond S., et al.
Published: (2018)

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

Supersonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle /
by: Ware, George M., et al.
Published: (1994)

YF-12 Experiments Symposium /
Published: (1978)

Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01 /
by: Foster, Gerald V.
Published: (1959)

Design and analysis tool for external-compression supersonic inlets /
by: Slater, John W.
Published: (2012)

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

Estimation of supersonic stage separation aerodynamics of winged-body launch vehicles using response surface methods /
by: Erickson, Gary E.
Published: (2010)

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

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

Transonic aerodynamic characteristics of a tailless fixed-wing supersonic transport model /
by: Ray, Edward J., et al.
Published: (1966)

Comparison of various supersonic turbine tip designs to minimize aerodynamic loss and tip heating /
by: Shyam, Vikram
Published: (2012)

Dynamic ground effect for a cranked arrow wing airplane /
by: Curry, Robert E.
Published: (1997)

Multifidelity analysis and optimization for supersonic design /
Published: (2010)

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)

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)

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

Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets /
by: Trefny, Charles J., et al.
Published: (1986)

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

Investigation of "6X" scramjet inlet configurations /
by: Alter, Stephen J.
Published: (2012)

A study of the sonic-boom characteristics of a blunt body at a Mach number of 6 /
by: Ashby, George C.
Published: (1980)

A System for aerodynamic design and analysis of supersonic aircraft /
by: Middleton, W. D. (Wilbur D.), 1931-, et al.
Published: (1980)

Subsonic investigation of a leading-edge boundary layer control suction system on a high-speed civil transport configuration /
by: Campbell, Bryan A.
Published: (1999)

New design concepts for high speed air transport /
Published: (1997)

Noise correction for supersonic inlet geometry /
by: Stephens, David B. (David Bruce)
Published: (2022)

Pilot comments for high speed research cycle 3 simulation study (LaRC.1) /
Published: (2000)

Flight tests of a supersonic natural laminar flow airfoil /
by: Frederick, Michael A.
Published: (2015)

Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63 /
by: Pittman, Jimmy L., et al.
Published: (1980)

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)

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)

Aerodynamic coefficients from aeroballistic range testing of deployed-and stowed-SIAD SFDT models /
by: Wilder, Michael C.
Published: (2017)

Evaluation of a technique to generate artificially thickened boundary layers in supersonic and hypersonic flows /
Published: (1991)

A rapid empirical method for estimating the gross takeoff weight of a high speed civil transport /
by: Mack, Robert J.
Published: (1999)

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

Focused and steady-state characteristics of shaped sonic boom signatures : prediction and analysis /
Published: (2011)