UNSTEADY AND STEADY AERODYNAMIC FORCES OF SLENDER DELTA WINGS ACCORDING TO THIN SHOCK LAYER THEORY

Journal article

Peer reviewed

H T Hemdan and W H Hui

Canadian aeronautics and space journal, Vol.23(4), pp.238-251

01/01/1977

Abstract

Engineering

Engineering, Aerospace

Science & Technology

Technology

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Title: UNSTEADY AND STEADY AERODYNAMIC FORCES OF SLENDER DELTA WINGS ACCORDING TO THIN SHOCK LAYER THEORY
Creators - without role: H T Hemdan
W H Hui
Publication Details: Canadian aeronautics and space journal, Vol.23(4), pp.238-251
Publisher: CANADIAN AERONAUT SPACE INST
Number of pages: 14
Identifiers: 9952065408331
Academic Unit: King Saud University
Language: English
Resource Type: Journal article