Conical shock-strength determination on low-sonic-boom aircraft model by doppler global velocimetry / Gregory C. Herring and James F. Meyers.

Author/creator Herring, Gregory C.
Other author Meyers, James F.
Other author Langley Research Center.
Format Electronic
Publication InfoHampton, Va. : National Aeronautics and Space Administration, Langley Research Center, [2011]
Description1 online resource (29 p.) : ill. (some col.)
Supplemental Contenthttps://purl.fdlp.gov/GPO/gpo13301

Variant title Conical shock strength determination on low sonic boom aircraft model by doppler global velocimetry
SeriesNASA/TM ; 2011-217052
NASA technical memorandum 217052. ^A467613
General noteTitle from title screen (viewed on Sept. 27, 2011).
General note"February 2011."
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (p. 16-18).
Funding informationSponsored by National Aeronautics and Space Administration 984754.02.07.07.11.03
GPO item number0830-D (online)
Govt. docs number NAS 1.15:2011-217052

Availability

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Electronic Resources Access Content Online ✔ Available