Flight services and aircraft access : active flow control vertical tail and insect accretion and mitigation flight test /

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

Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept /
by: Hahne, David E. (David Edgar)
Published: (1997)

Flight, wind-tunnel, and computational fluid dynamics comparison for cranked arrow wing (F-16XL-1) at subsonic and transonic speeds /
Published: (2001)

A comparison of pressure measurements between a full-scale and a 1/6-scale F/A-18 twin tail during buffet /
by: Moses, Robert W., et al.
Published: (1996)

Wind tunnel acoustic study of a propeller installed behind an airplane empennage : data report /
by: WiIby, J. F.
Published: (1985)

Fundamental ice crystal accretion physics studies /
Published: (2012)

Flight test results on the stability and control of the F-15 Quiet Spike aircraft /
by: Moua, Cheng M.
Published: (2012)

Mid-fidelity computational fluid dynamics analysis of the Elytron 4S UAV concept /
by: Koning, Witold J. F.
Published: (2018)

An experimental approach to a rapid propulsion and aeronautics concepts testbed /
by: McSwain, Robert G.
Published: (2020)

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

Wind-tunnel investigation of a flush airdata system at Mach numbers from 0.7 to 1.4 /
by: Larson, Terry J.
Published: (1990)

Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed /
by: Smith, Arthur F.
Published: (1985)

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

Subsonic dynamics of stardust sample return capsule /
by: Mitcheltree, Robert A. (Robert Alan), 1961-, et al.
Published: (1997)

Investigation of solid plume simulation criteria to produce flight plume effects on multibody configuration in wind tunnel tests /
by: Frost, Alonzo L.
Published: (1986)

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)

Experimental aeroelasticity history, status and future in brief /
by: Ricketts, Rodney H.
Published: (1990)

Rime ice accretion and its effect on airfoil performance /
by: Bragg, Michael B., 1954-
Published: (1982)

Scaling of lift degradation due to anti-icing fluids based upon the aerodynamic acceptance test /
by: Broeren, Andy P., et al.
Published: (2012)

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

Wind-tunnel and flight-test results for the measurements of flow variables at supersonic speeds using improved wedge and conical probes /
by: Bobbitt, Percy J.
Published: (2012)

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)

Locally linearized longitudinal and lateral-directional aerodynamic stability and control derivatives for the X-29A aircraft /
by: Budd, Gerald D.
Published: (1984)

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

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

Rotor CFD analysis at terrestrial and martian atmospheric densities /
by: Perez Perez, Brenda Natalia
Published: (2018)

Pressure probe designs for dynamic pressure measurements in a supersonic flow field /
by: Porro, A. Robert
Published: (2001)

Output measurement equations for flexible aircraft flight dynamics /
by: Grauer, Jared A., et al.
Published: (2018)

Isolated rotor forward flight testing at Martian atmospheric density data report /
by: Ament, Geoffrey A., et al.
Published: (2019)

1-by 1- foot supersonic wind tunnel sidewall flowfield compression plate study /
by: Peters, Christopher J. (Christopher John), et al.
Published: (2020)

A two-dimensional adaptive-wall test section with ventilated walls in the Ames 2- by 2-foot transonic wind tunnel /
by: Schairer, Edward T.
Published: (1989)

Supersonic wind tunnel tests of a half-axisymmetric 12⁰-spike inlet to a rocket-based combined-cycle propulsion system /
by: DeBonis, J. R.
Published: (2001)

Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system /
by: DeBonis, James R., et al.
Published: (2001)

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)

Experimental and computational sonic boom assessment of Boeing N+2 low boom models /
by: Durston, D. A.
Published: (2015)

Lewis Icing Research Tunnel test of the aerodynamic effects of aircraft ground deicing/anti-icing fluids /
by: Runyan, L. James
Published: (1992)