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Engine/airframe integration for waverider cruise vehiclesEngine-airframe integrated hypersonic waveriders have been optimized previously for both cruising flight and accelerators using inverse design flowfields to provide desirable aerodynamic performance and inlet properties. With engine installation, cruisers retain the high L/D advantages of the basic waverider form. To provide an understanding of waverider optimizer trends, an analytical development is presented which includes the presentation of a simplified model of a generic waverider shape. The model is shown to have good agreement with computational results, and it is used to demonstrate engineering tradeoffs in L/D, volume, and volume efficiency. Based on the demonstrated performance trends, and considering the desirability of uniform inlet flow, an improved waverider shape for engine-airframe integration is proposed using a hybrid cone-wedge generating flowfield.
Document ID
19930039257
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lewis, Mark J.
(NASA Ames Research Center Moffett Field, CA, United States)
Takashima, Naruhisa
(Maryland Univ. College Park, United States)
Date Acquired
August 16, 2013
Publication Date
January 1, 1993
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 93-0507
Report Number: AIAA PAPER 93-0507
Meeting Information
Meeting: AIAA, Aerospace Sciences Meeting and Exhibit
Location: Reno, NV
Country: United States
Start Date: January 11, 1993
End Date: January 14, 1993
Sponsors: AIAA
Accession Number
93A23254
Funding Number(s)
CONTRACT_GRANT: NCA2-611
CONTRACT_GRANT: NAG1-1192
Distribution Limits
Public
Copyright
Other

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