Evaluation of gritting strategies for high angle of attack using wind tunnel and flight test data for the F/A-18 /

Overview of HATP experimental aerodynamics data for the baseline F/A-18 configuration : High-Angle-of-Attack Technology Conference /
Published: (1996)

Extraction of lateral-directional stability and control derivatives for the basic F-18 aircraft at high angles of attack /
by: Iliff, Kenneth W., et al.
Published: (1997)

Navier-Stokes, flight, and wind tunnel flow analysis for the F/A-18 aircraft.
by: Ghaffari, Farhad
Published: (1994)

F-18 High Alpha Research Vehicle surface pressures : initial in-flight results and correlation with flow visualization and wind-tunnel data /
by: Fisher, David F.
Published: (1990)

Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers /
by: Stolike, Patrick C.
Published: (1996)

Low-speed wind tunnel tests of two waverider configuration models /
by: Pegg, Robert J.
Published: (1995)

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

Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft /
by: Klein, Vladislav
Published: (1997)

F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack : contract NAS 3-26617 /
Published: (1997)

Results of aerothermodynamic and boundary layer transition testing of 0.0362-Scale X-38 (Rev 3.1) vehicle in NASA Langley 20-inch Mach 6 tunnel /
Published: (1997)

Role of wind tunnels and computer codes in the certification and qualification of rotorcraft for flight in forecast icing /
by: Flemming, Robert J.
Published: (1994)

Exploratory investigation of forebody strakes for yaw control of a generic fighter with a symmetric 60⁰ half-angle chine forebody /
by: Ross, Holly M.
Published: (1997)

Effect of in-flight ice accretion on the performance of a multi-element airfoil /
Published: (1995)

Pseudosteady-state analysis of nonlinear aircraft maneuvers /
by: Young, John W. (John Worth), 1934-, et al.
Published: (1980)

Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack /
by: Cobleigh, Brent R., et al.
Published: (2001)

Comparison of X-31 flight and ground-based yawing moment asymmetries at high angles of attack /
by: Cobleigh, Brent R.
Published: (2001)

Lateral and longitudinal aerodynamic stability and control parameters of the basic vortex flap research aircraft as determined from flight test data /
by: Suit, William T. (William Tull), 1937-
Published: (1986)

Low-speed wind-tunnel investigation of the stability and control characteristics of a series of flying wings with sweep angles of 50⁰.
by: Fears, Scott P.
Published: (1995)

Review of the Aerodynamic Acceptance Test and application to anti-icing fluids testing in the NRC propulsion and icing wind tunnel /
by: Broeren, Andy P., et al.
Published: (2012)

The Altitude wind tunnel (AWT)--a unique facility for propulsion system and adverse weather testing /
by: Chamberlin, Roger
Published: (1985)

System dynamic analysis of a wind tunnel model with applications to improve aerodynamic data quality : a dissertation ... /
by: Buehrle, Ralph David
Published: (1997)

In-flight aerodynamic measurements of an iced horizontal tailplane /
by: Ratvasky, Thomas P.
Published: (1999)

Research and applications in aeroelasticity and structural dynamics at the NASA Langley Research Center /
by: Abel, Irving
Published: (1997)

Investigation of materials for boundary layer control in a supersonic wind tunnel /
by: Braafladt, Alexander C., et al.
Published: (2013)

Fourth High Alpha Conference, NASA Dryden Flight Research Center, Edwards, California, July 12-14, 1994.
Published: (1994)

A study of large droplet ice accretion in the NASA Lewis IRT at near-freezing conditions; Pt. 2.
by: Addy, Harold E., Jr., 1960-
Published: (1997)

Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers /
by: Stoliker, Patrick C., et al.
Published: (1996)

Aerodynamic parameters of an advanced fighter aircraft estimated from flight data : preliminary results /
by: Klein, Vladislav
Published: (1989)

Aerodynamic parameters of an advanced fighter aircraft estimated from flight data : preliminary results /
by: Klein, Vladislav
Published: (1989)

Flow-visualization study of the X-29A aircraft at high angles of attack using a 1/48-scale model /
by: Cotton, Stacey J.
Published: (1994)

Summary of the 2017 blockage test in the 10- by 10-foot supersonic wind tunnel /
by: Pastor-Barsi, Christine, 1982-, et al.
Published: (2018)

Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack /
by: Walsh, Kevin R.
Published: (1997)

Wind-tunnel development of an SR-71 aerospike rocket flight test configuration /
Published: (1996)

F-15B/flight test fixture II : a test bed for flight research /
by: Richwine, David M.
Published: (1996)

Estimation of aircraft nonlinear unsteady parameters from wind tunnel data /
by: Klein, Vladislav
Published: (1998)

Estimation of aircraft nonlinear unsteady parameters from wind tunnel data /
by: Klein, Vladislav, et al.
Published: (1998)