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Performance Evaluation Method for Dissimilar Aircraft Designs. Technical Report NASA Reference Publication RP-1042, Research Engineering, NASA Dryden Flight Research Center

Walker, Harold J. (1979) Performance Evaluation Method for Dissimilar Aircraft Designs. Technical Report NASA Reference Publication RP-1042, Research Engineering, NASA Dryden Flight Research Center.

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Abstract

A rationale is presented for using the square of the wingspan rather than the wing reference area as a basis for nondimensional comparisons of the aerodynamic and performance characteristics of aircraft that differ substantially in planform and loading. Working relationships are developed and illustrated through application to several categories of aircraft covering a range of Mach numbers from 0.60 to 2.00. For each application, direct comparisons of drag polars, lift-to-drag ratios, and maneuverability are shown for both nondimensional systems. The inaccuracies that may arise in the determination of aerodynamic effciency based on reference area are noted. Span loading is introduced independently in comparing the combined effects of loading and aerodynamic efficiency on overall performance. Performance comparisons are made for the NACA research aircraft, lifting bodies, century-series fighter aircraft, F-111A aircraft with conventional and supercritical wings, and a group of superconic aircraft including the B-58 and XB-70 bomber aircraft. An idealized configuration is included in each category to serve as a standard for comparing overall efficiency.

EPrint Type:Other
Keywords:Performance evaluation methods, Research aircraft, B-58, F-102A
Subjects:Aircraft/Project: XF-92
Aircraft/Project: F-100
Aircraft/Project: F-4
Aircraft/Project: D-558-II
Aircraft/Project: YF-102
Aircraft/Project: X-15
Aircraft/Project: F-111
Aircraft/Project: X-1
Aircraft/Project: F-104
Aircraft/Project: X-3
Aircraft/Project: X-24A
Aircraft/Project: F-106
Aircraft/Project: Multiple Aircraft
Aircraft/Project: X-5
Aircraft/Project: X-24B
(01 - 09) Aeronautics: (01) Aeronautics - General
Aircraft/Project: Oblique-Wing
Aircraft/Project: XB-70
Aircraft/Project: M2-F2
Aircraft/Project: HL-10
ID Code:661
Deposited On:10 Febuary 2006
Additional Information:72 pages.
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