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4D dynamic required navigation performance final report

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speeds

Boppe, Charles W.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987. 1987

Analysis of NLR configurations using OCM for pilot modeling

Drajeske, M. H.
West Lafayette, Ind. : Purdue University, School of Aeronautics and Astronautics ; [Washington, D.C. : National Aeronautics and Space Administration, 1987] 1987

Dynamic ground-effect measurements on the F-15 STOL and Maneuver Technology Demonstrator (S/MTD) con

Kemmerly, Guy T.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990. 1990

Economic evaluation of flying-qualities design criteria for a transport configured with relaxed stat

Sliwa, Steven M., author.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1980. 1980-

Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temper

Reardon, Lawrence R.
[Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1989. 1989

Experimental and computational sonic boom assessment of Lockheed-Martin N+2 low boom models

Cliff, Susan E., author.
Moffett Field, CA : National Aeronautics and Space Administration, Ames Research Center, January 2015. 2015-

Feasibility study for a microwave-powered ozone sniffer aircraft.

[Washington, D.C. : National Aeronautics and Space Administration, 1990] 1990

Final report for the advanced concept studies for supersonic commercial transports entering service

Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2010] 2010

Fuselage design for a specified Mach-sliced area distribution

Barger, Raymond L.
[Washington, DC] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1990. 1990

High speed research system study advanced flight deck configuration effects

Swink, Jay R.
Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1992] 1992

N+3 advanced concept studies for supersonic commercial transport aircraft entering service in the 20

Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011] 2011

NASA/USRA high altitude reconnaissance aircraft.

[Washington, D.C. : National Aeronautics and Space Administration, 1990] 1990

Numerical study of three-dimensional separation and flow control at a wing-body junction progress re

Lakshmanan, Balakrishnan, 1957-
Norfolk, Va. : Department of Mechanical Engineering and Mechanics, College of Engineering and Technology, Old Dominion University ; Hampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [1989] 1989

Prediction of forces and moments for flight vehicle control effectors

Hampton, VA : National Aeronautics and Space Administration, Langley Research Center, [1990] 1990

Study for prediction of rotor/wake/fuselage interference

Clark, D. R.
Redmond, WA : Analytical Methods, Inc. ; Moffett Field, Calif : National Aeronautics and Space Administration, Ames Research Center, [1985] 1985

Supersonic flow computations for an ASTOVL aircraft configuration phase 2, part 2

Ramakrishnan, Sekaripuram.
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1990. 1990