Aircraft Configurations

135 books
Supersonic civil airplane study and designSamson H. Cheung

Supersonic civil airplane study and design

Samson H. Cheung

1995No page data
Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configurationDale R. Satran
⏱ 56m

Wind-tunnel investigation of the flight characteristics of a Canard general-aviation airplane configuration

Dale R. Satran

198656 pp.
The lift-fan aircraftW. H. Deckert

The lift-fan aircraft

W. H. Deckert

1995No page data
The flying diamond, a joined aircraft configuration design contest.Unknown Author

The flying diamond, a joined aircraft configuration design contest.

Unknown Author

1988No page data
Supersonic wing and wing-body shape optimization using an adjoint formulationJames Reuther

Supersonic wing and wing-body shape optimization using an adjoint formulation

James Reuther

1995No page data
Supersonic flow computations for an ASTOVL aircraft configurationSekaripuram Ramakrishnan
⏱ 40m

Supersonic flow computations for an ASTOVL aircraft configuration

Sekaripuram Ramakrishnan

199040 pp.
Preliminary design and analysis of procedures for the numerical generation of 3D block-structured gridsJ. W. Boerstoel
⏱ 1h 18m

Preliminary design and analysis of procedures for the numerical generation of 3D block-structured grids

J. W. Boerstoel

198678 pp.
Multiple application propfan study (MAPS)Unknown Author

Multiple application propfan study (MAPS)

Unknown Author

1989No page data
HOMAR:a computer code for generating homotopic grids using algebraic relationsAnutosh Moitra

HOMAR:a computer code for generating homotopic grids using algebraic relations

Anutosh Moitra

1989No page data
Unified theory for aircraft handling qualities and adverse aircraft--pilot couplingR. A. Hess

Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling

R. A. Hess

1997No page data
Investigation into the impact of agility in conceptual fighter designR. M. Engelbeck

Investigation into the impact of agility in conceptual fighter design

R. M. Engelbeck

1995No page data
Unified theory for aircraft handling qualities and adverse aircraft--pilot couplingR. A. Hess

Unified theory for aircraft handling qualities and adverse aircraft--pilot coupling

R. A. Hess

1997No page data
Tailless aircraft performance improvementsIrving Louis Ashkenas

Tailless aircraft performance improvements

Irving Louis Ashkenas

1989No page data
Utilization of an agility assessment module in analysis and optimization of preliminary fighter configurationAngelen Ngan

Utilization of an agility assessment module in analysis and optimization of preliminary fighter configuration

Angelen Ngan

1996No page data
Aerodynamic analysis for aircraft with nacelles, pylons, and winglets at transonic speedsCharles W. Boppe

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

Charles W. Boppe

1987No page data
A comparison of interactional aerodynamics methods for a helicopter in low speed flightUnknown Author

A comparison of interactional aerodynamics methods for a helicopter in low speed flight

Unknown Author

1998No page data
Flight-testing of the self-repairing flight control system using the F-15 highly integrated digital electronic control flight research facilityJames F. Stewart
⏱ 13m

Flight-testing of the self-repairing flight control system using the F-15 highly integrated digital electronic control flight research facility

James F. Stewart

199013 pp.
The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplaneFrank W. Burcham
⏱ 12m

The value of early flight evaluation of propulsion concepts using the NASA F-15 research airplane

Frank W. Burcham

198712 pp.
A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areasRobert J. Mack

A semiempirical method for obtaining fuselage normal areas from fuselage mach sliced areas

Robert J. Mack

1990No page data
High speed research system studyJay R. Swink

High speed research system study

Jay R. Swink

1992No page data
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