Comparison of hotshot tunnel force, pressure heat-transfer and shock shape data with shock tunnel data

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086 0 ⊔ ‡aD 301.45/33-2:64-001
100 1 ⊔ ‡aEdenfield, E. E., ‡eauthor.
245 1 0 ‡aComparison of hotshot tunnel force, pressure heat-transfer and shock shape data with shock tunnel data / ‡cby E.E. Edenfield.
264 ⊔ 1 ‡aArnold Air Force Station, Tennessee : ‡bArnold Engineering Development Center, Air Force Systems Command, United States Air Force, ‡c1964.
300 ⊔ ⊔ ‡a25 pages : ‡billustrations, ‡c28 cm
336 ⊔ ⊔ ‡atext ‡btxt ‡2rdacontent
337 ⊔ ⊔ ‡aunmediated ‡bn ‡2rdamedia
338 ⊔ ⊔ ‡avolume ‡bnc ‡2rdacarrier
490 0 ⊔ ‡aAEDC-TDR ; ‡v64-001
500 ⊔ ⊔ ‡a"January 1964."
504 ⊔ ⊔ ‡aIncludes bibliographic references (pages 7-9).
520 ⊔ ⊔ ‡aComparison is made of force, pressure, heat-transfer, and shock shape data from tests in the AEDC-VKF hotshot tunnels and in the Cornell Aeronautical Laboratory 48 Inch Shock Tunnel. Several cone models of varying bluntness were tested through an angle-of-attack range of 0 to 40 deg at each facility. Excellent agreement of the hotshot and the shock tunnel data is shown. (Author).
536 ⊔ ⊔ ‡aReport prepared by ARO, Inc., under Air Force Contract No. ‡bAF 40(600)-1000.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aHypersonic wind tunnels.
650 ⊔ 0 ‡aCone ‡xAerodynamics.
650 ⊔ 0 ‡aShock tunnels.
710 2 ⊔ ‡aARO, Inc., ‡esponsor.
710 2 ⊔ ‡aArnold Engineering Development Center, ‡esponsor.
710 1 ⊔ ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing body.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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