The effect of airflow cooling on a scramjet: a preliminary assessment
Author:
Affiliation:
1. Victoria University, Wellington, New Zealand and APECS Ltd, 3 Hawkley Hurst, Hawkley, Hants GU33 6NS, UK
Publisher
The Royal Society
Subject
General Physics and Astronomy,General Engineering,General Mathematics
Link
https://royalsocietypublishing.org/doi/pdf/10.1098/rsta.1999.0434
Reference5 articles.
1. Lundin B. T. 1949 Analysis of turbojet thrust augmentation cycles. Preprint 223 Institute of Aeronautical Science.
2. Moteurs thermiques;Roy M. M.;C. R. Acad. Sci.,1946
3. Roy M. M. 1958 Propulsion supersonique par turboréacteurs et par statoréacteurs. Proc. 1st Int. Cong. on Aeronautical Science Madrid. New York: Pergamon.
4. Townend L. H. 1966 Ramjet propulsion for hypersonic aircraft. Euromech 3 Aachen. RAE TM Aero 917.
5. Whittle F. 1953 Jet ch. 43. London: Frederick Muller.
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