Nonlinear aerodynamic wing design /
| Main Author: | Bonner, Ellwood (Author) |
|---|---|
| Corporate Author: | Langley Research Center |
| Format: | Government Document eBook |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration, Scientific and Technical Information Branch,
December 1985.
|
| Series: | NASA contractor report ;
NASA CR-3950. |
| Subjects: | |
| Online Access: | https://purl.fdlp.gov/GPO/gpo106459 |
Similar Items
Comparison of Theodorsen's unsteady aerodynamic forces with double lattice generalized aerodynamic forces /
by: Perry, Boyd
Published: (2017)
by: Perry, Boyd
Published: (2017)
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)
by: Wood, Richard M., et al.
Published: (1985)
Investigation of active flow control to improve aerodynamic performance of oscillating wings /
by: Narducci, Robert P.
Published: (2014)
by: Narducci, Robert P.
Published: (2014)
Numerical study of steady and unsteady canard-wing-body aerodynamics /
by: Tu, Eugene L.
Published: (1996)
by: Tu, Eugene L.
Published: (1996)
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)
by: Wood, Richard M., et al.
Published: (1985)
Wind tunnel results of the aerodynamic performance of a 1/8-scale model of a twin-engine transport with multi-element wing /
by: Laflin, Brenda E. Gile, et al.
Published: (1997)
by: Laflin, Brenda E. Gile, et al.
Published: (1997)
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)
by: Erickson, Gary E.
Published: (2013)
Fuselage design for a specified Mach-sliced area distribution /
by: Barger, Raymond L.
Published: (1990)
by: Barger, Raymond L.
Published: (1990)
An aerodynamic tradeoff study of the scissor wing configuration /
by: Selberg, Bruce P.
Published: (1990)
by: Selberg, Bruce P.
Published: (1990)
Swept-wing ice accretion characterization and aerodynamics /
by: Broeren, Andy P.
Published: (2013)
by: Broeren, Andy P.
Published: (2013)
Supersonic aerodynamic characteristics of some reentry concepts for angles of attack to 90⁰ /
by: Spearman, M. Leroy
Published: (1985)
by: Spearman, M. Leroy
Published: (1985)
Commercial cargo derivative study of the advanced hybrid wing body configuration with over-wing engine nacelles /
by: Hooker, John R., et al.
Published: (2017)
by: Hooker, John R., et al.
Published: (2017)
Experimental surface pressure data obtained on 65 ° delta wing across Reynolds number and Mach number ranges /
by: Chu, Julio, et al.
Published: (1996)
by: Chu, Julio, et al.
Published: (1996)
Enabling rapid and robust structural analysis during conceptual design /
by: Eldred, Lloyd B., et al.
Published: (2015)
by: Eldred, Lloyd B., et al.
Published: (2015)
Application of a Navier-Stokes solver to the analysis of multielement airfoils and wings using multizonal grid techniques /
by: Jones, Kenneth M., et al.
Published: (1995)
by: Jones, Kenneth M., et al.
Published: (1995)
Aerodynamic effects of simulated ice accretion on a generic transport model /
Published: (2012)
Published: (2012)
Natural laminar flow flight experiments on a swept wing business jet- boundary layer stability analyses /
by: Rozendaal, R. A.
Published: (1986)
by: Rozendaal, R. A.
Published: (1986)
Low-Reynolds number aerodynamics of an 8.9 percent scale semispan swept wing for assessment of icing effects /
by: Broeren, Andy P.
Published: (2017)
by: Broeren, Andy P.
Published: (2017)
Nacelle integration to reduce the sonic boom of aircraft designed to cruise at supersonic speeds /
by: Mack, Robert J.
Published: (1999)
by: Mack, Robert J.
Published: (1999)
Design verification and fabrication of active control systems for the DAST ARW-2 high aspect ratio wing /
by: McGehee, C. R.
Published: (1986)
by: McGehee, C. R.
Published: (1986)
The behavior of a stitched composite large-scale multi-bay pressure box /
by: Jegley, Dawn C.
Published: (2016)
by: Jegley, Dawn C.
Published: (2016)
Numerical study of three-dimensional separation and flow control at a wing-body junction : progress report for the period ended April 30, 1989 /
by: Lakshmanan, Balakrishnan, 1957-
Published: (1989)
by: Lakshmanan, Balakrishnan, 1957-
Published: (1989)
Low-speed, high-lift aerodynamic characteristics of slender, hypersonic accelerator-type configurations /
by: Gatlin, Gregory M. (Gregory Michael)
Published: (1989)
by: Gatlin, Gregory M. (Gregory Michael)
Published: (1989)
Design of a slotted, natural-laminar-flow airfoil for a transport aircraft /
by: Somers, Dan M.
Published: (2019)
by: Somers, Dan M.
Published: (2019)
Damage arresting composites for shaped vehicles : phase II final report /
Published: (2011)
Published: (2011)
Full potential methods for analysis/design of complex aerospace configurations /
by: Shankar, Vijaya, et al.
Published: (1986)
by: Shankar, Vijaya, et al.
Published: (1986)
NASA N+3 subsonic fixed wing silent efficient low-emissions commercial transport (SELECT) vehicle study, revision a /
Published: (2010)
Published: (2010)
Calculation of vortex-flap aerodynamic characteristics /
by: Lan, C. Edward (Chuan-Tau Edward), 1935-, et al.
Published: (1985)
by: Lan, C. Edward (Chuan-Tau Edward), 1935-, et al.
Published: (1985)
Application of approximate unsteady aerodynamics for flutter analysis /
by: Pak, Chan-gi
Published: (2010)
by: Pak, Chan-gi
Published: (2010)
Effects of wing sweep on boundary-layer transition for a smooth F-14A wing at Mach numbers from 0.700 to 0.825 /
by: Anderson, Bianca T. (Bianca Trujillo)
Published: (1990)
by: Anderson, Bianca T. (Bianca Trujillo)
Published: (1990)
Experimental and theoretical aerodynamic characteristics of a high-lift semispan wing model /
by: Applin, Zachary T.
Published: (1990)
by: Applin, Zachary T.
Published: (1990)
Full-field reconstruction of structural deformations and loads from measured strain data on a wing test article using the inverse finite element method /
by: Miller, Eric J., et al.
Published: (2016)
by: Miller, Eric J., et al.
Published: (2016)
Computation of flow over a drag prediction workshop wing/body transport configuration using CFL3D /
by: Rumsey, C. L. (Christopher Lockwood), 1961-
Published: (2001)
by: Rumsey, C. L. (Christopher Lockwood), 1961-
Published: (2001)
Robust airfoil optimization to achieve consistent drag reduction over a mach range /
by: Li, Wu
Published: (2001)
by: Li, Wu
Published: (2001)
Experimental investigation of aeroelastic deformation of slender wings at supersonic speeds using a video model deformation measurement technique /
by: Erickson, Gary E.
Published: (2013)
by: Erickson, Gary E.
Published: (2013)
Effects of wing sweep on in-flight boundary-layer transition for a laminar flow wing at Mach numbers from 0.60 to 0.79 /
by: Anderson, Bianca T. (Bianca Trujillo)
Published: (1990)
by: Anderson, Bianca T. (Bianca Trujillo)
Published: (1990)
The flying diamond, a joined aircraft configuration design contest. final report.
Published: (1988)
Published: (1988)
Missile aerodynamics for ascent and re-entry /
by: Watts, G. L., et al.
Published: (2012)
by: Watts, G. L., et al.
Published: (2012)
Super cooled large droplet analysis of several geometries using LEWICE3D version 3 /
by: Bidwell, Colin S.
Published: (2011)
by: Bidwell, Colin S.
Published: (2011)
Use of constrained optimization in the conceptual design of a medium-range subsonic transport /
by: Sliwa, Steven M.
Published: (1980)
by: Sliwa, Steven M.
Published: (1980)