Author: Edwin J. SaltzmanPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
Book Description
Base Pressure Coefficients Obtained from the X-15 Airplane for Mach Numbers Up to 6
Author: Edwin J. SaltzmanPublisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 56
Book Description
NASA Technical Note
Author: Scientific and Technical Aerospace Reports
Author: Monthly Catalog of United States Government Publications
Author: Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1284
Book Description
Comparison of Wind-tunnel and Flight-measured Base Pressures from the Sharp-leading-edge Upper Vertical Fin of the X-15 Airplane for Turbulent Flow at Mach Numbers from 1.5 to 5.0
Author: Sheryll Goecke PowersPublisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 44
Book Description
Monthly Catalog of United States Government Publications, Cumulative Index
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : United States
Languages : en
Pages : 1250
Book Description
Wind-tunnel Force and Pressure Tests of Rocket-engine Nozzle Extensions on the 0.0667-scale X-15-2 Model at Supersonic and Hypersonic Speeds
Author: Earl J. MontoyaMonthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1248
Book Description
Flight-measured Base Pressure Coefficients for Thick Boundary-layer Flow Over an Aft-facing Step for Mach Numbers from 0.4 to 2.5
Author: Sheryll A. GoeckePublisher:
ISBN:
Category : B-70 bomber
Languages : en
Pages : 44
Book Description
Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1208
Book Description