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1. PROGRAM AND CHARTS FOR DETERMINING SHOCK TUBE EXPANSION TUBE AND EXPANSION TUNNEL FLOW QUANTITIES FOR REAL AIR

by Miller,Charles G | Wilder,Sue E.

Material type: book Book Description: 278.Publisher: Nasa, Washington, D.C. 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: TR TND-7752] (1).

2. REAL-AIR DATA-REDUCTION PROCEDURES BASED ON FLOW PARAMETERS MEASURED IN THE TEST SECTION OF SUPERSONIC AND HYPERSONIC FACILITIES

by Miller Iii,Charles G | Wilder,Sue E.

Material type: book Book Description: 90.Publisher: Nasa, Washington, D.C. 1972Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-6618 -] (1).

3. REAL-HELIUM HYPERSONIC FLOW PARAMETERS FOR PRESSURES TO 3600 ATMOSPHERES AND TEMPERATURES TO 15 000 (DEGRE) K

by Miller Iii,Charles G | Wilder,Sue E.

Material type: book Book Description: 41.Publisher: Nasa, Washington, D.C. 1968Availability: Items available for reference: PK Kelkar Library, IIT Kanpur [Call number: NASA TN D-4869] (1).

4. Program and charts for determining shock tube expansion tube and expansion tunnel flow quantities for real air [NASA TN D-7752]

by Miller, Charles G | Wilder, Sue E.

Material type: book Book; Format: print ; Literary form: not fiction Description: 278p.Publisher: Washington, D. C. National Aeronautics and Space Administration 1975Availability: Items available for reference: PK Kelkar Library, IIT Kanpur (1).

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