Economic evaluation of flying-qualities design criteria for a transport configured with relaxed static stability /

High-Alpha handling qualities flight research on the NASA F/A-18 High Alpha Research Vehicle /
by: Wichman, Keith D.
Published: (1996)

Commercial cargo derivative study of the advanced hybrid wing body configuration with over-wing engine nacelles /
by: Hooker, John R., et al.
Published: (2017)

Artificial neural networks applications : from aircraft design optimization to orbiting spacecraft on-board environment monitoring /
by: Jules, Kenol, et al.
Published: (2002)

Numerical experience with a class of algorithms for nonlinear optimization using inexact function and gradient information /
by: Carter, Richard G.
Published: (1989)

Propulsion and airframe aerodynamic interactions of supersonic V/STOL configurations, Phase I /
by: Mraz, M. R., et al.
Published: (1985)

N+3 advanced concept studies for supersonic commercial transport aircraft entering service in the 2030-2035 period /
Published: (2011)

Aircraft of the future /
by: Yeger, S.
Published: (1985)

Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) configuration /
by: Kemmerly, Guy T.
Published: (1990)

High speed research system study : advanced flight deck configuration effects /
by: Swink, Jay R.
Published: (1992)

Structural dynamic model obtained from flight for use with piloted simulation and handling qualities analysis /
by: Powers, Bruce G.
Published: (1996)

Tandem fan applications in advanced STOVL fighter configurations /
by: Zola, Charles L.
Published: (1984)

Compressive testing of stitched frame and stringer alternate configurations /
by: Leone, Frank A., et al.
Published: (2016)

Benefit assessment for metroplex tactical runway configuration management (mTRCM) in a simulated environment /
by: Phojanamongkolkij, Nipa
Published: (2015)

Airfoil dynamic stall and rotorcraft maneuverability /
by: Bousman, William G.
Published: (2000)

Airfoil dynamic stall and rotorcraft maneuverability /
by: Bousman, William G. (William Giles)
Published: (2000)

Supersonic flow computations for an ASTOVL aircraft configuration : phase 2, part 2 /
by: Ramakrishnan, Sekaripuram
Published: (1990)

Fuselage design for a specified Mach-sliced area distribution /
by: Barger, Raymond L.
Published: (1990)

Waverider. final report, 1987-1988.
Published: (1988)

Full potential methods for analysis/design of complex aerospace configurations /
by: Shankar, Vijaya, et al.
Published: (1986)

Low-speed static and dynamic force tests of a generic supersonic cruise fighter configuration /
by: Hahne, David E. (David Edgar)
Published: (1989)

Parametric study of a canard-configured trasport using conceptual design optimization /
by: Arbuckle, P. Douglas, et al.
Published: (1985)

Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds /
by: Boppe, Charles W.
Published: (1987)

Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds /
by: Boppe, Charles W.
Published: (1987)

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)

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)

4D dynamic required navigation performance final report /
Published: (2011)

Advanced technology subsonic transport study : N+3 technologies and design concepts /
Published: (2011)

Documentation of the tangent linear and adjoint models of the Relaxed Arakawa-Schubert moisture parameterization package of the NASA GEOS-1 GCM (version 5.2) /
by: Yang, Weiyu, et al.
Published: (1997)

Autonomous RPRV navigation, guidance and control /
by: Johnston, Donald E., et al.
Published: (1983)

Low-speed stability and control test of a "double-bubble" transport configuration /
by: Vicroy, Dan D.
Published: (2017)

Advanced Rotorcraft Transmission Program /
by: Bill, Robert C.
Published: (1990)

NASA/USRA high altitude reconnaissance aircraft.
Published: (1990)

Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models /
by: Cliff, Susan E.
Published: (2015)

Operational overview for UAS integration in the NAS project flight test series 3 /
by: Valkov, Steffi B., et al.

Numerical study of steady and unsteady canard-wing-body aerodynamics /
by: Tu, Eugene L.
Published: (1996)

Silent aircraft initiative concept risk assessment /
by: Nickol, Craig L.
Published: (2008)