A simple analytical model to describe the impact of wing on the flowfield over the tail in subsonic flow-Reference-Cited by-同舟云学术

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A simple analytical model to describe the impact of wing on the flowfield over the tail in subsonic flow

Published:2018-04 Issue: Volume:75 Page:88-98
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Davari Ali R.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Airplane body (non-lifting system) drag and influence on lifting system. influence of the airplane body on the wings;Wieselsburger,1934

2. Experimental and Theoretical Study of the Interference at Low Speed Between Slender Bodies and Triangular Wings;Hopkins,1953

3. Wing–Body Interference at Supersonic Speeds with an Application to Combinations with Rectangular Wings;Nielson,1952

4. Interference between wing and body at supersonic speeds-theory and numerical application;Ferrari;J. Aeronaut. Sci.,1948

5. The Wing–Body Problem for Linearized Supersonic Flow;Morikawa,1949

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