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James D. Knittel

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Publication

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Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 6. Wing Chordwise Pressure Distribution - Nacelles Off.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9 Volume 8. Wing Chordwise Pressure Distributions, Effects of: Nacelles, Flaps, Spoilers, Sideslip, and Reynolds Number. Part 1.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 9. Horizontal Stabilzer Section and Total Surface Aerodynamic Coefficients, Chordwise Pressure Distributions.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 5. Wing Net Chordwise Pressure distribution and Isobars - Nacelles on. Part 1.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 10. Horizontal Stabilizer Net Chordwise Pressure Distributions and Isobars.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination At Mach Numbers from 0.3 to 2.9. Volume 7. Wing Net Chordwise Pressure Distributions and Isobars - Nacelles Off.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 2. Comparisons of Theory and Experiment.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 3. Wing Section and Total Surface Aerodynamic Coefficients.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 13. Body, Nacelles, and Leading and Trailing Edge Flap Load Distributions.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

Archive | 1972

Pressure Distributions on a Delta Wing - Horizontal Stabilizer Combination at Mach Numbers from 0.3 to 2.9. Volume 1. Summary Report.

Marjorie E. Manro; Johan P. Moulijn; James D. Knittel

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