Experimental work on the aerodynamics of integrated slender wings for supersonic flight

Author:

Squire L.C.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Aerospace Engineering

Reference52 articles.

1. Some considerations of aircraft shapes and their aerodynamics for flight at supersonic speeds;Küchemann,1961

2. The aerodynamic design of aircraft;Küchemann,1978

3. An analysis of some performance aspects of various types of aircraft designed to fly over different ranges at different speeds;Küchemann;Prog. in Aerospace Sci.,1968

4. On the aerodynamic design of slender wings;Maskell;J. Roy. Aero. Soc.,1959

5. Some aspects of the low-speed and supersonic aerodynamics of lifting slender wings;Spence,1962

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1. Aerodynamic Efficiency of SCV Configurations;Essentials of Supersonic Commercial Aircraft Conceptual Design;2020-06-05

2. Flat Wings in Inviscid Supersonic Flow;Essentials of Supersonic Commercial Aircraft Conceptual Design;2020-06-05

3. The discovery and prediction of vortex flow aerodynamics;The Aeronautical Journal;2019-06

4. Propulsion System Requirements for Long Range, Supersonic Aircraft;Journal of Fluids Engineering;2005-03-08

5. Leading-edge vortex breakdown for wing planforms with the same slenderness ratio;Journal of Aircraft;1994-05

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